Supersonic Combustion

122 books
Fuel-rich catalytic combustion of a high density fuelTheodore A. Brabbs
⏱ 11m

Fuel-rich catalytic combustion of a high density fuel

Theodore A. Brabbs

199311 pp.
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
Ignition delay and characteristic reaction length in shock induced supersonic combustionT. Gary Yip
⏱ 10m

Ignition delay and characteristic reaction length in shock induced supersonic combustion

T. Gary Yip

198910 pp.
Progress toward shock enhancement of supersonic combustion processesFrank E. Marble

Progress toward shock enhancement of supersonic combustion processes

Frank E. Marble

1987No page data
A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustorJames C. McDaniel

A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor

James C. McDaniel

1986No page data
Diagnostics in supersonic combustionY. M. Timnat

Diagnostics in supersonic combustion

Y. M. Timnat

1987No page data
A review of supersonic combustion research at AEDC with hypersonic applicationsPhilip M. Rubins
⏱ 11m

A review of supersonic combustion research at AEDC with hypersonic applications

Philip M. Rubins

199311 pp.
Conceptual model of turbulent flameholding for scramjet combustorsPaul W. Huber
⏱ 33m

Conceptual model of turbulent flameholding for scramjet combustors

Paul W. Huber

198033 pp.
Multidisciplinary analysis of a hypersonic engineUnknown Author

Multidisciplinary analysis of a hypersonic engine

Unknown Author

2002No page data
A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injectionN. D. Domel
⏱ 11m

A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection

N. D. Domel

199111 pp.
Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstreamMarshall C. Burrows
⏱ 25m

Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream

Marshall C. Burrows

197325 pp.
Noncircular jet dynamics in supersonic combustionE. Gutmark

Noncircular jet dynamics in supersonic combustion

E. Gutmark

1987No page data
Evaluation of parallel injector configurations for supersonic combustionG. Burton Northam
⏱ 14m

Evaluation of parallel injector configurations for supersonic combustion

G. Burton Northam

198914 pp.
Mixing enhancement in a supersonic combustorJ. Philip Drummond
⏱ 15m

Mixing enhancement in a supersonic combustor

J. Philip Drummond

198915 pp.
Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gasH. L. Beach
⏱ 10m

Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas

H. L. Beach

197210 pp.
Analysis of external burning on inclined surfaces in supersonic flowJoseph A. Schetz
⏱ 10m

Analysis of external burning on inclined surfaces in supersonic flow

Joseph A. Schetz

199110 pp.
Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstreamR. Clayton Rogers
⏱ 10m

Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream

R. Clayton Rogers

197310 pp.
Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight ProgramAlexander S. Roudakov

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program

Alexander S. Roudakov

1998No page data
Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulationLawrence D. Huebner
⏱ 46m

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation

Lawrence D. Huebner

199346 pp.
Flow establishment in a generic scramjet combustorP. A. Jacobs
⏱ 38m

Flow establishment in a generic scramjet combustor

P. A. Jacobs

199038 pp.
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