Ramjet Engines

160 books
Practical intake aerodynamic designE. L. Goldsmith
⏱ 7h 14m

Practical intake aerodynamic design

E. L. Goldsmith

1993434 pp.
Turbofan forced mixer-nozzle internal flowfieldRobert W. Paterson

Turbofan forced mixer-nozzle internal flowfield

Robert W. Paterson

1982No page data
Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6Louis L. Steers

Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

Louis L. Steers

1979No page data
Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzlesHilary Kozlowski
⏱ 3h 1m

Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles

Hilary Kozlowski

1978181 pp.
Comparison of combustion efficiencies for ramjet enginesJürgen W. Bergmann

Comparison of combustion efficiencies for ramjet engines

Jürgen W. Bergmann

1984No page data
Thermodynamische Stromungsbeschreibung eines Staustrahltriebwerks mit Unterschallverbrennung zur Bestimmung der Triebwerkskrafte und MomenteFrans G. J. Kremer
⏱ 2h 35m

Thermodynamische Stromungsbeschreibung eines Staustrahltriebwerks mit Unterschallverbrennung zur Bestimmung der Triebwerkskrafte und Momente

Frans G. J. Kremer

1991155 pp.
Some fundamentals on the performance of ramjets with subsonic and supersonic combustionH Wittenberg
⏱ 3h 9m

Some fundamentals on the performance of ramjets with subsonic and supersonic combustion

H Wittenberg

2000189 pp.
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.
Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6Louis L Steers

Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

Louis L Steers

1979No page data
Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraftBarbara S. Esker

Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft

Barbara S. Esker

1993No page data
Control of aircraft and missile powerplantsAlbert J. Sobey
⏱ 7h 12m

Control of aircraft and missile powerplants

Albert J. Sobey

1963432 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
Numerical study of chemically reacting flows using an LU schemeJian-Shun Shuen

Numerical study of chemically reacting flows using an LU scheme

Jian-Shun Shuen

1988No page data
Comparison of combustion efficiencies for ramjet enginesJürgen W Bergmann

Comparison of combustion efficiencies for ramjet engines

Jürgen W Bergmann

1984No page data
The design and performance estimates for the propulsion module for the booster of a TSTO vehicleChristopher Snyder

The design and performance estimates for the propulsion module for the booster of a TSTO vehicle

Christopher Snyder

1991No page data
Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡miVladimir Isaakovich Polikovskiĭ
⏱ 4h 20m

Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi

Vladimir Isaakovich Polikovskiĭ

1965260 pp.
A parametric study of a gas-generator airturbo ramjet (ATR)Christopher Snyder

A parametric study of a gas-generator airturbo ramjet (ATR)

Christopher Snyder

1986No page data
Contribution à l'etude aérodynamique du statoréacteur subsoniqueO. Schrenk
⏱ 49m

Contribution à l'etude aérodynamique du statoréacteur subsonique

O. Schrenk

195149 pp.
Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭVitaliĭ Mitrofanovich Dorofeev
⏱ 3h 40m

Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭ

Vitaliĭ Mitrofanovich Dorofeev

1961220 pp.
Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭVladimir Stepanovich Zuev
⏱ 6h 7m

Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭ

Vladimir Stepanovich Zuev

1971367 pp.
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