Combustion Temperature

68 books
A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSEC. Y. Tsai

A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE

C. Y. Tsai

1998No page data
NASA Lewis Research Center's Preheated Combustor and Materials Test FacilitySteve A. Nemets

NASA Lewis Research Center's Preheated Combustor and Materials Test Facility

Steve A. Nemets

1995No page data
High intensity combustors, steady isobaric combustionSigmar Wittig
⏱ 7h 54m

High intensity combustors, steady isobaric combustion

Sigmar Wittig

2002474 pp.
NASA Lewis Research Center's combustor test facilities and capabilitiesJean Bianco

NASA Lewis Research Center's combustor test facilities and capabilities

Jean Bianco

1995No page data
Kinetics, equilibria and performance of high temperature systemsUnknown Author
⏱ 3h 45m

Kinetics, equilibria and performance of high temperature systems

Unknown Author

1960225 pp.
Finite-rate water condensation in combustion-heated wind tunnelsWayne D. Erickson
⏱ 1h 9m

Finite-rate water condensation in combustion-heated wind tunnels

Wayne D. Erickson

198869 pp.
High-temperature optical window designNorman Roeloffs

High-temperature optical window design

Norman Roeloffs

1995No page data
Combustion for Material SynthesisAlexander S. Rogachev
⏱ 7h 4m

Combustion for Material Synthesis

Alexander S. Rogachev

2014424 pp.
The Sandia Laboratory Combustion Simulation facilityKennith L Goin
⏱ 27m

The Sandia Laboratory Combustion Simulation facility

Kennith L Goin

197927 pp.
The Sandia Laboratory Combustion Simulation facilityKennith L. Goin
⏱ 27m

The Sandia Laboratory Combustion Simulation facility

Kennith L. Goin

197927 pp.
Flame temperatures in an internal combustion engine measured by spectral line reversalAlbert Eby Hershey
⏱ 50m

Flame temperatures in an internal combustion engine measured by spectral line reversal

Albert Eby Hershey

193350 pp.
High-temperature durability considerations for HSCT combustorNathan S. Jacobson
⏱ 16m

High-temperature durability considerations for HSCT combustor

Nathan S. Jacobson

199216 pp.
An analysis of particle-temperature modulations induced by pulsed-laser sourcesW. L. Flower
⏱ 30m

An analysis of particle-temperature modulations induced by pulsed-laser sources

W. L. Flower

197930 pp.
Detailed mechanism for oxidation of benzeneDavid A. Bittker
⏱ 30m

Detailed mechanism for oxidation of benzene

David A. Bittker

199030 pp.
Ignition and combustion of bulk metals at normal, elevated, and reduced gravityM. C. Branch

Ignition and combustion of bulk metals at normal, elevated, and reduced gravity

M. C. Branch

1995No page data
Thermal decomposition and combustion of explosives and propellantsG. B. Manelis
⏱ 6h 16m

Thermal decomposition and combustion of explosives and propellants

G. B. Manelis

2003376 pp.
Testing of wrought iridium/chemical vapor deposition rhenium rocketBrian D. Reed

Testing of wrought iridium/chemical vapor deposition rhenium rocket

Brian D. Reed

1997No page data
Self-propagating high-temperature synthesis of materialsL. De Luca
⏱ 5h 37m

Self-propagating high-temperature synthesis of materials

L. De Luca

2002337 pp.
Characteristics of vaporizing cryogenic sprays for rocket combustion modelingRobert D. Ingebo

Characteristics of vaporizing cryogenic sprays for rocket combustion modeling

Robert D. Ingebo

1994No page data
Tverdoplamennoe gorenieAleksandr Grigorʹevich Merzhanov
⏱ 3h 58m

Tverdoplamennoe gorenie

Aleksandr Grigorʹevich Merzhanov

2000238 pp.
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