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COMBUSTION INSTABILITY

  • Combustion instability
  • Physical phenomena

    Combustion instabilities are physical phenomena occurring in a reacting flow (e.g., a flame) in which some perturbations, even very small ones, grow and

    Combustion instability

    Combustion instability

    Combustion_instability

  • Combustion
  • Chemical reaction between a fuel and oxygen

    the combustion temperature and thus reduce the NOx emissions; however, running the combustion lean makes it very susceptible to combustion instability. The

    Combustion

    Combustion

    Combustion

  • Rocket engine
  • Non-airbreathing engine used to propel a missile or vehicle

    the supersonic pressure wave formed in the combustion chamber may destroy the engine. Combustion instability was also a problem during Atlas development

    Rocket engine

    Rocket engine

    Rocket_engine

  • Thermo-acoustic instability
  • unsteady heat release process. This instability is very relevant in combustion instabilities in systems such as rocket engines, etc. A very simple mechanism

    Thermo-acoustic instability

    Thermo-acoustic_instability

  • LGM-25C Titan II
  • US ICBM, in service from 1962 to 1987

    delayed by a month when the Titan's right engine experienced severe combustion instability at ignition that caused the entire thrust chamber to break off of

    LGM-25C Titan II

    LGM-25C Titan II

    LGM-25C_Titan_II

  • Pogo oscillation
  • Type of vibration in a rocket engine

    vibration in liquid-propellant rocket engines caused by combustion instability. The unstable combustion results in variations in engine thrust, causing variation

    Pogo oscillation

    Pogo_oscillation

  • Rocketdyne F-1
  • Rocket engine used on the Saturn V rocket

    at least through 1965. Early development tests revealed serious combustion instability problems which sometimes caused catastrophic failure. Initially

    Rocketdyne F-1

    Rocketdyne F-1

    Rocketdyne_F-1

  • Charles Duke
  • American astronaut and lunar explorer (born 1935)

    survive. Testing at the White Sands Missile Range in 1966 indicated combustion instability. George Low, the Apollo Spacecraft Program manager, convened a committee

    Charles Duke

    Charles Duke

    Charles_Duke

  • Pyrotechnic composition
  • Non-explosives producing heat, light and sound

    Aluminium – most common fuel in many classes of mixtures, also a combustion instability suppressant. Less energy per mass than carbon but less gas evolution

    Pyrotechnic composition

    Pyrotechnic_composition

  • Atlas LV-3B
  • American space launch vehicle

    standard D-series valve for reliability and weight-saving reasons. Combustion instability was a repeated problem in static firing tests of the MA-2 engines

    Atlas LV-3B

    Atlas LV-3B

    Atlas_LV-3B

  • Titan II GLV
  • American expendable launch system

    were removed. Because the second stage engine had had issues with combustion instability, it was equipped with baffled injectors. The first stage was loaded

    Titan II GLV

    Titan II GLV

    Titan_II_GLV

  • Rotating detonation engine
  • Type of rocket engine

    from theoretical studies on detonation waves and rocket engine combustion instability. Experimental observation and analysis first occurred in 1950s in

    Rotating detonation engine

    Rotating detonation engine

    Rotating_detonation_engine

  • Diffusive–thermal instability
  • Instrinsic flame instability

    Darrieus–Landau instability Kuramoto–Sivashinsky equation Clavin–Garcia equation Double diffusive convection (1944). Theory of Combustion and Detonation

    Diffusive–thermal instability

    Diffusive–thermal_instability

  • William Sirignano
  • American aerospace engineer (born 1938)

    fluid dynamicist. He is known for his theoretical work on resolving combustion instability problems in the Rocketdyne F-1 engine during the Apollo program

    William Sirignano

    William_Sirignano

  • Ascent propulsion system
  • Apollo Lunar Module rocket engine

    injector system, at the request of NASA, when Bell could not solve combustion instability problems. The LMAE traces its origin to the earlier Bell Aerosystems

    Ascent propulsion system

    Ascent propulsion system

    Ascent_propulsion_system

  • Pintle injector
  • Propellant injection device for a rocket engine

    based on regular injectors, and will very rarely present acoustic combustion instabilities, because a pintle injector tends to create a self-stabilizing flow

    Pintle injector

    Pintle injector

    Pintle_injector

  • Engine knocking
  • Problem in internal combustion engines

    fuel–air mix itself, and due to Rayleigh–Taylor instability (resulting from the hot, low-density combustion gasses expanding into the relatively cold and

    Engine knocking

    Engine knocking

    Engine_knocking

  • Hybrid-propellant rocket
  • Rocket engine that uses both liquid / gaseous and solid fuel

    ), density, or both. Combustion instabilities – Hybrid rockets do not typically exhibit high frequency combustion instabilities that plague liquid rockets

    Hybrid-propellant rocket

    Hybrid-propellant rocket

    Hybrid-propellant_rocket

  • RD-0110
  • Soviet (later Russian) rocket engine

    certification testing, high frequency combustion instabilities at start up were still observed. Even though the start instabilities were relatively rare at 1 in

    RD-0110

    RD-0110

    RD-0110

  • Gary Flandro
  • American aerospace engineer

    Marble and Fred E. Culick, with a thesis on the "Sergeant rocket combustion instability problem and the associated roll torque puzzle". In 1964, Flandro

    Gary Flandro

    Gary Flandro

    Gary_Flandro

  • Solid rocket booster
  • Solid propellant motor used to augment the thrust of a rocket

    aerodynamic stresses. Additional failure modes include bore choking and combustion instability. Failure of an O-ring seal on the Challenger space shuttle's right

    Solid rocket booster

    Solid rocket booster

    Solid_rocket_booster

  • Cape Canaveral Launch Complex 11
  • Former missile test launch site in Florida, US

    1960, which suffered combustion instability and exploded on the pad. Although no specific cause for the combustion instability could be determined, the

    Cape Canaveral Launch Complex 11

    Cape Canaveral Launch Complex 11

    Cape_Canaveral_Launch_Complex_11

  • Darrieus–Landau instability
  • Intrinsic instability in flames

    flame instability that occurs in premixed flames, caused by density variations due to thermal expansion of the gas produced by the combustion process

    Darrieus–Landau instability

    Darrieus–Landau_instability

  • SM-65E Atlas
  • Variant of the U.S. Atlas missile

    ignition that required no hold-down time on the pad to prevent combustion instability. The booster engines had separate gas generators unlike the Atlas

    SM-65E Atlas

    SM-65E Atlas

    SM-65E_Atlas

  • Nuri (rocket)
  • First South Korean orbital launch vehicle developed domestically

    three-stage engine combustion test facility and a combustor combustion test facility. However, the problem of combustion instability in the KRE-075 burner

    Nuri (rocket)

    Nuri (rocket)

    Nuri_(rocket)

  • R. I. Sujith
  • Professor of Aerospace Engineering

    transition from the state of combustion noise to the state of thermo-acoustic instability. He suggested that combustion noise exhibits multifractality

    R. I. Sujith

    R. I. Sujith

    R._I._Sujith

  • RD-170
  • Soviet (now Russian) rocket engine, the most powerful in the world

    engine designers, including Valentin P. Glushko, faced problems of combustion instability while designing bigger thrust chambers. At that time, they solved

    RD-170

    RD-170

    RD-170

  • Michelson–Sivashinsky equation
  • In combustion, the Michelson–Sivashinsky equation describes the evolution of a premixed flame front, subjected to the Darrieus–Landau instability, in the

    Michelson–Sivashinsky equation

    Michelson–Sivashinsky_equation

  • SM-65D Atlas
  • First operational version of the U.S. Atlas missile

    experienced combustion instability again, this time in the B-2 engine. The first indication of trouble was a pressure surge in the B-2 combustion chamber

    SM-65D Atlas

    SM-65D Atlas

    SM-65D_Atlas

  • Kosmos-3M
  • Russian space launch vehicle

    sabotage was ruled out. The failure was traced to high-frequency combustion instability, which had been a problem with the RD-219 engine and was also responsible

    Kosmos-3M

    Kosmos-3M

  • Ariane 1
  • European medium-lift space launch vehicle (1979–1986)

    in a failure shortly after takeoff, which had been caused by a combustion instability that had occurred in one of the Viking first stage engines. The

    Ariane 1

    Ariane 1

    Ariane_1

  • Chugging
  • Topics referred to by the same term

    street fundraising a form of rapid drinking. a type of rocket engine combustion instability when broken down palm muting, guitar technique This disambiguation

    Chugging

    Chugging

  • Luna E-1 No.1
  • Soviet space probe (Luna 1958A)

    caused considerable damage to Site 1/5, was traced to high frequency combustion instability in the strap-on RD-107 engines, something that would become a persistent

    Luna E-1 No.1

    Luna E-1 No.1

    Luna_E-1_No.1

  • Soyuz-U
  • Soyuz rocket design variant

    RD-117/118 engines to mitigate issues like in-flight vibration and combustion instability. Complete adoption of the Soyuz-U was not achieved until 1977, when

    Soyuz-U

    Soyuz-U

    Soyuz-U

  • Regenerative cooling (rocketry)
  • Passing cold propellant through tubes around a rocket engine to cool it

    poor conductors. This boundary layer can be destroyed however by combustion instabilities, and wall failure can follow very soon afterwards. The boundary

    Regenerative cooling (rocketry)

    Regenerative_cooling_(rocketry)

  • Electric vehicle
  • Vehicle propelled fully or mostly by electricity

    limited range hindered mass adoption throughout the 20th century. Internal combustion engines were the dominant propulsion mechanisms for cars and trucks for

    Electric vehicle

    Electric vehicle

    Electric_vehicle

  • Richtmyer–Meshkov instability
  • The Richtmyer–Meshkov instability (RMI) occurs when two fluids of different density are impulsively accelerated. Normally this is by the passage of a

    Richtmyer–Meshkov instability

    Richtmyer–Meshkov_instability

  • YF-1
  • Chinese liquid rocket engine

    development had great trouble with combustion instabilities and it took a long time to have a reliable combustion. The basic engine has been used since

    YF-1

    YF-1

  • Valentin Glushko
  • Soviet rocket engineer (1908–1989)

    much more time and money to design. Glushko never did overcome the combustion instability problems of large rocket engines using kerosene propellants; his

    Valentin Glushko

    Valentin Glushko

    Valentin_Glushko

  • Forman A. Williams
  • American academic

    premixed turbulent flame as a wrinkled flame. The classification of Combustion instabilities was first introduced by Williams and Barrère in 1969. He introduced

    Forman A. Williams

    Forman A. Williams

    Forman_A._Williams

  • Viking (rocket engine)
  • Engines used in EU rocket Ariane

    failure (on second Ariane 1 flight 23 May 1980) was due to a chamber combustion instability. The vehicle had lost an attitude control and broke up. Several

    Viking (rocket engine)

    Viking (rocket engine)

    Viking_(rocket_engine)

  • Hybrid rocket fuel regression
  • off large fragments, greatly reduces combustion efficiency and potentially contributing to combustion instability. Although it is much harder to predict

    Hybrid rocket fuel regression

    Hybrid_rocket_fuel_regression

  • Thierry Poinsot
  • French researcher

    , « A review of active control methods for combustion instabilities », Progress in Energy and Combustion Science, (1992) 19, p. 1-29 Candel S.M. et Poinsot

    Thierry Poinsot

    Thierry_Poinsot

  • IIT Madras
  • Research Institute in Chennai, Tamil Nadu, India

    advanced research initiatives will focus on cryo-tank thermodynamics, combustion instability in hybrid rockets, and spacecraft thermal management. E-Summit by

    IIT Madras

    IIT_Madras

  • KRE-075
  • South Korean rocket engine

    months. There was an issue with the combustion instability of the engine, and at the time, the combustion instability issue had been resolved to some extent

    KRE-075

    KRE-075

    KRE-075

  • Turbofan
  • Airbreathing jet engine designed to provide thrust by driving a fan

    afterburning can approach stoichiometric temperatures as limited by combustion instabilities. The first production afterburning turbofan engine was the Pratt

    Turbofan

    Turbofan

    Turbofan

  • SM-64 Navaho
  • 1950s supersonic intercontinental cruise missile

    performance. The Germans were never able to get this working due to combustion instability and continued using the earlier design in spite of lower performance

    SM-64 Navaho

    SM-64 Navaho

    SM-64_Navaho

  • James Arthur Nicholls
  • American aerospace engineer and detonation engine pioneer

    Michigan known for his work in detonation physics, rocket engine combustion instability, and rotating detonation engines. He was the first researcher to

    James Arthur Nicholls

    James_Arthur_Nicholls

  • Williams spray equation
  • Frequency Combustion Instability,”." Eighth Symposium (International) on Combustion. Williams and Wilkins. 1962. Tanasawa, Y. "On the Combustion Rate of

    Williams spray equation

    Williams_spray_equation

  • Saverio "Sonny" Morea
  • American aerospace engineer and aviator

    F-1 engine program, overseeing a $1 billion budget. Morea called combustion instability, a major issue in the development of the F-1, "the biggest problem

    Saverio "Sonny" Morea

    Saverio_"Sonny"_Morea

  • Hermes program
  • United States Army missile research program

    great influence on future engine development in the United States. Combustion instability problems delayed engine development. Hermes A-1 components such

    Hermes program

    Hermes program

    Hermes_program

  • UH 25
  • Liquid rocket propellant

    one of the four Viking engines on the first stage developed a combustion instability which led to an engine fire, subsequent explosion and destruction

    UH 25

    UH_25

  • Edward W. Price (engineer)
  • Test Station (NOTS), where he made contributions to ignition, combustion instabilities, fuel components, and the "T-burner" method of testing. After 30

    Edward W. Price (engineer)

    Edward_W._Price_(engineer)

  • Ben Zinn
  • Israeli-American soccer player and academic

    dissertation titled "A theoretical study of nonlinear transverse combustion instability in liquid propellant rocket motors." He began his forty-year association

    Ben Zinn

    Ben_Zinn

  • Joseph Majdalani
  • Lebanese-American professor

    wave propagation. Both have been used in frameworks for modeling combustion instability in rocket systems. Majdalani has also developed a mathematical framework

    Joseph Majdalani

    Joseph Majdalani

    Joseph_Majdalani

  • Westinghouse J46
  • Turbojet aircraft engine family

    original electronic control system, compressor/turbine mismatches, combustion instability and control issues at altitude leading to compressor stalling The

    Westinghouse J46

    Westinghouse J46

    Westinghouse_J46

  • Clavin–Garcia equation
  • gases. Combustion science and technology, 46(3-6), 167-193. Truffaut, J. M., & Searby, G. (1999). Experimental study of the Darrieus-Landau instability on

    Clavin–Garcia equation

    Clavin–Garcia_equation

  • Space Race (TV series)
  • 2005 British TV series or programme

    Braun has continuing difficulties with the Saturn V, especially combustion instability in the large F-1 engine, but these are ultimately overcome almost

    Space Race (TV series)

    Space_Race_(TV_series)

  • Mercury-Atlas 8
  • Manned NASA spacecraft

    original pyrotechnic igniter. This would eliminate problems with combustion instability and allow the booster to be released immediately upon attaining

    Mercury-Atlas 8

    Mercury-Atlas 8

    Mercury-Atlas_8

  • Véronique (rocket)
  • 1950s French sounding rocket

    immediately upon launch. Initially, the rocket motor suffered from combustion instability, which became a leading cause of early launch failures; furthermore

    Véronique (rocket)

    Véronique (rocket)

    Véronique_(rocket)

  • Aerojet LR87
  • American rocket engine family used on Titan missile first stages

    Though the earlier tests with the LR87 were terminated due to combustion instabilities and funding restraints development of gelled fuel and oxidizers

    Aerojet LR87

    Aerojet LR87

    Aerojet_LR87

  • Ammonium perchlorate
  • Chemical compound

    a major component of ammonium perchlorate composite propellant. Its instability has involved it in accidents such as the PEPCON disaster, and has been

    Ammonium perchlorate

    Ammonium perchlorate

    Ammonium_perchlorate

  • List of University of Michigan alumni
  • Allen F. Donovan (M.S.), worked with NASA to solve the problem of combustion instability that affected Project Mercury, and later on the pogo oscillation

    List of University of Michigan alumni

    List_of_University_of_Michigan_alumni

  • December 1963
  • Month of 1963

    made, including problems related to longitudinal oscillations, combustion instability, and engine improvement. Died: Maurice Baker, 35, a former Dallas

    December 1963

    December 1963

    December_1963

  • Aimee Morgans
  • British engineer

    but efforts to mitigate these emissions results in combustion instabilities. These instabilities occur due to unsteady burning of gases, which creates

    Aimee Morgans

    Aimee_Morgans

  • Whittle Laboratory
  • Research laboratory in Cambridge, England

    Cambridge University Engineering Department and who had developed the combustion chamber in Sir Frank Whittle jet engine used in the first British jet

    Whittle Laboratory

    Whittle Laboratory

    Whittle_Laboratory

  • Daniel Klute
  • American rocket scientist and chemical engineer

    serious instability problem during combustion that would sometimes cause catastrophic failure. In October, 1962, Dr. Klute presided over the Combustion Stability

    Daniel Klute

    Daniel_Klute

  • Deflagration to detonation transition
  • Type of explosion

    in which a combustion process transitions from deflagration (subsonic flame propagation) to a detonation (supersonic shock-coupled combustion). In a deflagration

    Deflagration to detonation transition

    Deflagration_to_detonation_transition

  • Staged combustion
  • Staged combustion is a method used to reduce the emission of nitrogen oxides (NOx) during combustion. There are two methods for staged combustion: air staged

    Staged combustion

    Staged combustion

    Staged_combustion

  • Ensemble de Lancement Vega
  • Launch pad at the Guiana Space Centre

    23 May 1980 14:29 Ariane 1 CAT-2 and secondary payloads Failure Combustion instability led to first stage failure and loss of vehicle during launch. 4

    Ensemble de Lancement Vega

    Ensemble de Lancement Vega

    Ensemble_de_Lancement_Vega

  • George H. Markstein
  • American combustion scientist (1911–2011)

    George H. Markstein was a combustion scientist, who has made pioneering contributions to flame theory and detonations. George H. Markstein was born in

    George H. Markstein

    George_H._Markstein

  • List of R-7 launches (1960–1964)
  • (8K72L) L1-10 LC-1/5, Baikonur Failure Korabl-Sputnik (Vostok) Combustion instability caused engine failure and explosion in the Blok G strap-on T+23

    List of R-7 launches (1960–1964)

    List_of_R-7_launches_(1960–1964)

  • Ebrahim Victory
  • Iranian mechanical engineer and author (1933–2025)

    S. Air Force, silent propulsion systems for the U.S. Navy, and combustion instability in rockets for NASA. He also worked for Johnson and Johnson and

    Ebrahim Victory

    Ebrahim Victory

    Ebrahim_Victory

  • Liquid-propellant rocket
  • Rocket engine that uses liquid fuels and oxidizers

    propellant prior to injection into the combustion chamber. Although many other features were used to ensure that instabilities could not occur, later research

    Liquid-propellant rocket

    Liquid-propellant rocket

    Liquid-propellant_rocket

  • September 1963
  • Month of 1963

    injectors, after development flights showed that the engine had combustion instability. The redesign took 18 months. On the same day, Manned Spacecraft

    September 1963

    September 1963

    September_1963

  • Pressure gain combustion
  • Unsteady state combustion process

    Pressure gain combustion (PGC) is the unsteady state process used in gas turbines in which gas expansion caused by heat release is constrained. First developed

    Pressure gain combustion

    Pressure gain combustion

    Pressure_gain_combustion

  • Turing pattern
  • Concept from evolutionary biology

    thermal diffusion coefficient. In combustion literature, Turing instability is referred to as diffusive–thermal instability.[citation needed] The original

    Turing pattern

    Turing pattern

    Turing_pattern

  • Vanguard SLV-1
  • Failed rocket launch

    in the second stage engine thrust chamber due to high-frequency combustion instability at engine shutdown. On subsequent flights, the second stage was

    Vanguard SLV-1

    Vanguard SLV-1

    Vanguard_SLV-1

  • List of R-7 launches (1957–1959)
  • E stage. Blok D engine failed at liftoff due to high frequency combustion instability and broke off the stack. The rest of the vehicle flew until T+40

    List of R-7 launches (1957–1959)

    List_of_R-7_launches_(1957–1959)

  • Contact explosive
  • Substance which explodes when exposed to small amounts of energy

    instead of explode because they must come into contact with oxygen in the combustion reaction. However, if the compound already contains both the oxidant and

    Contact explosive

    Contact explosive

    Contact_explosive

  • Ionization instability
  • An ionization instability is any one of a category of plasma instabilities which is mediated by electron-impact ionization. In the most general sense,

    Ionization instability

    Ionization_instability

  • White phosphorus
  • Chemical compound

    upon ingestion and phossy jaw from chronic ingestion or inhalation. The combustion of this form has a characteristic garlic odor, and samples are commonly

    White phosphorus

    White phosphorus

    White_phosphorus

  • Cape Canaveral Launch Complex 13
  • Former rocket launch site in Florida, USA

    occurred, the launch of Missile 51D in March 1960, which suffered combustion instability within seconds of launch. The Atlas fell back onto LC-13 in a huge

    Cape Canaveral Launch Complex 13

    Cape Canaveral Launch Complex 13

    Cape_Canaveral_Launch_Complex_13

  • Eddy break-up model
  • Model in combustion

    model (EBU) is used in combustion engineering. Combustion modeling has a wide range of applications. In most of the combustion systems, fuel and oxygen

    Eddy break-up model

    Eddy_break-up_model

  • Béla Karlovitz
  • Hungarian-American engineer, inventor

    he is the author of many publications on turbulent flames and combustion instabilities. He was the head of the Flame Research Section, Explosives and

    Béla Karlovitz

    Béla_Karlovitz

  • Theodore von Kármán bibliography
  • Technology, Tech. Rep. 16. Kármán, Th. von (1956). "Some remarks on combustion instability in rockets". AGARD Paper. Kármán, Th. von; Driscoll, B. J. (1956)

    Theodore von Kármán bibliography

    Theodore von Kármán bibliography

    Theodore_von_Kármán_bibliography

  • Reaction–diffusion system
  • Type of mathematical model

    R(u) = u(1 − u)e-β(1-u) and 0 < β < ∞ (Zeldovich number) that arises in combustion theory, and its particular degenerate case with R(u) = u2 − u3 that is

    Reaction–diffusion system

    Reaction–diffusion system

    Reaction–diffusion_system

  • Rocket engine nozzle
  • Type of propelling nozzle

    of the de Laval type) used in a rocket engine to expand and accelerate combustion products to high supersonic velocities. Simply: propellants pressurized

    Rocket engine nozzle

    Rocket engine nozzle

    Rocket_engine_nozzle

  • 1980 in spaceflight
  • Amsat-DE Intended: Molniya Amateur radio First stage failure due to combustion instability in main engine; first launch conducted by Arianespace 26 May 18:20:39

    1980 in spaceflight

    1980 in spaceflight

    1980_in_spaceflight

  • List of Atlas launches (1960–1969)
  • 1960-03-11 00:36 Atlas D 51D CCAFS LC-13 ICBM test Suborbital Failure Combustion instability in B-1 engine. Missile fell back onto the pad and exploded. 1960-04-08

    List of Atlas launches (1960–1969)

    List_of_Atlas_launches_(1960–1969)

  • List of Ariane launches (1979–1989)
  • Feurrad AMSAT-3A CAT-2 GTO Failure Failed to reach orbit due to combustion instability during first stage burn. 19 June 1981, 12:33 Ariane 1 L-03 Meteosat

    List of Ariane launches (1979–1989)

    List_of_Ariane_launches_(1979–1989)

  • Suzuki GSX series
  • Range of motorcycles

    cylinder hemispherical combustion chamber with domed piston design of the GS engine, to a four-valve per cylinder Twin Swirl Combustion Chamber (TSCC) with

    Suzuki GSX series

    Suzuki GSX series

    Suzuki_GSX_series

  • Wassim Michael Haddad
  • Lebanese-Greek-American mathematician

    disturbances. His results have been applied to combustion systems to suppress the effects of thermoacoustic instabilities in gas turbine engines as well as propulsion

    Wassim Michael Haddad

    Wassim Michael Haddad

    Wassim_Michael_Haddad

  • Octane rating
  • Standard measure of the performance of an engine or aviation fuel

    standard measure of a fuel's ability to withstand compression in an internal combustion engine without causing engine knocking. The higher the octane number,

    Octane rating

    Octane_rating

  • Cool flame
  • Flame with temperature below about 400 °C

    engine knock – the undesirable, erratic, and noisy combustion of low-octane fuels in internal combustion engines. Cool flames were accidentally discovered

    Cool flame

    Cool_flame

  • Spoil tip
  • Pile built of accumulated spoil

    high proportion of hydrocarbons or coal dust. Spontaneous subterranean combustion may result, which can be followed by surface fires. In some coal mining

    Spoil tip

    Spoil tip

    Spoil_tip

  • Rocket propellant
  • Chemical or mixture used in a rocket engine

    being accelerated by the pressure of the combusting gases against the combustion chamber and nozzle, not by "pushing" against the air behind or below it

    Rocket propellant

    Rocket propellant

    Rocket_propellant

  • Paul Clavin
  • French scientist

    French scientist at Aix-Marseille University, working in the field of combustion and statistical mechanics. He is the founder of Institute for Research

    Paul Clavin

    Paul_Clavin

  • Reacting Gas Dynamics Laboratory
  • concentrated solar thermal energy through thermochemical conversion and combustion. The RGD receives funding from a number of sources both public and private

    Reacting Gas Dynamics Laboratory

    Reacting_Gas_Dynamics_Laboratory

  • Pulverized coal-fired boiler
  • Type of boiler

    using pulverised fuel is to use the whole volume of the furnace for the combustion of solid fuels. Coal is ground to the size of a fine grain, mixed with

    Pulverized coal-fired boiler

    Pulverized_coal-fired_boiler

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Online names & meanings

  • Lala
  • Girl/Female

    Hawaiian American Latin Slavic Spanish

    Lala

    Equivalent of English Lara: famous;cheerful.

  • Ammara |
  • Girl/Female

    Muslim

    Ammara |

    Shining star

  • Waydell
  • Boy/Male

    British, English, Scandinavian

    Waydell

    Medieval Given Name from Scandinavian Mythology; Water Crossing

  • Makrand | மகரஂத
  • Boy/Male

    Tamil

    Makrand | மகரஂத

    Honey

  • AKINYI
  • Female

    African

    AKINYI

    born in the morning (?).

  • Barnett
  • Surname or Lastname

    English

    Barnett

    English : habitational name from various places, for example Chipping (High) Barnet, East Barnet, and Friern Barnet in Greater London, named with Old English bærnet ‘place cleared by burning’ (a derivative of bærnan ‘to burn’, ‘to set light to’).English : from a medieval personal name, a variant of Bernard.

  • Geetasri | கீதாஸரீ
  • Girl/Female

    Tamil

    Geetasri | கீதாஸரீ

    Bhagvat Gita

  • Pragyan
  • Boy/Male

    Hindu

    Pragyan

    Greater knowledge, Wisdom

  • Giuditta
  • Girl/Female

    Italian

    Giuditta

    Praised.

  • SAPPHIRA
  • Female

    Greek

    SAPPHIRA

    (Σάπφιρα) Greek name SAPPHIRA means "sapphire." In the bible, this is the name of the wife of Ananias.

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  • Ambustion
  • n.

    A burn or scald.

  • Combustious
  • a.

    Inflammable.

  • Accelerograph
  • n.

    An apparatus for studying the combustion of powder in guns, etc.

  • Smoulder
  • v. i.

    To burn and smoke without flame; to waste away by a slow and supressed combustion.

  • Combustion
  • n.

    The combination of a combustible with a supporter of combustion, producing heat, and sometimes both light and heat.

  • Soot
  • n.

    A black substance formed by combustion, or disengaged from fuel in the process of combustion, which rises in fine particles, and adheres to the sides of the chimney or pipe conveying the smoke; strictly, the fine powder, consisting chiefly of carbon, which colors smoke, and which is the result of imperfect combustion. See Smoke.

  • Blaze
  • n.

    A stream of gas or vapor emitting light and heat in the process of combustion; a bright flame.

  • Midfeather
  • n.

    A vertical water space in a fire box or combustion chamber.

  • Spark
  • n.

    A small particle of fire or ignited substance which is emitted by a body in combustion.

  • Combustion
  • n.

    Violent agitation; confusion; tumult.

  • Combustion
  • n.

    The state of burning.

  • Fire
  • n.

    The evolution of light and heat in the combustion of bodies; combustion; state of ignition.

  • Ashes
  • n. pl.

    The earthy or mineral particles of combustible substances remaining after combustion, as of wood or coal.

  • Flame
  • n.

    To burn with a flame or blaze; to burn as gas emitted from bodies in combustion; to blaze.

  • Fume
  • n.

    To smoke; to throw off fumes, as in combustion or chemical action; to rise up, as vapor.

  • Deflagrator
  • n.

    A form of the voltaic battery having large plates, used for producing rapid and powerful combustion.

  • Gaslight
  • n.

    The light yielded by the combustion of illuminating gas.

  • Fire
  • n.

    Fuel in a state of combustion, as on a hearth, or in a stove or a furnace.

  • Cineration
  • n.

    The reducing of anything to ashes by combustion; cinefaction.

  • Stinkball
  • n.

    A composition of substances which in combustion emit a suffocating odor; -- used formerly in naval warfare.