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ramjet engines

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View Turbofan forced mixer-nozzle internal flowfield By Robert W. Paterson

Turbofan forced mixer-nozzle internal flowfield

Turbofan forced mixer-nozzle internal flowfield

By Robert W. Paterson

View CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system By Ing Chuang

CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system

CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system

By Ing Chuang

View Analysis of a new rocket-based combined-cycle engine concept at low speed By S. Yungster

Analysis of a new rocket-based combined-cycle engine concept at low speed

Analysis of a new rocket-based combined-cycle engine concept at low speed

By S. Yungster

View Control of aircraft and missile powerplants By Albert J. Sobey

Control of aircraft and missile powerplants

Control of aircraft and missile powerplants

By Albert J. Sobey

View Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control By A. B. Blair

Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

By A. B. Blair

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

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

By Louis L. Steers

View Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles By Hilary Kozlowski

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

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

By Hilary Kozlowski

View Virtualʹnye aviadvigateli By A. N. Zhukov

Virtualʹnye aviadvigateli

Virtualʹnye aviadvigateli

By A. N. Zhukov

View Analysis of internal flow in a ventral nozzle for STOVL aircraft By C. Frederic Smith

Analysis of internal flow in a ventral nozzle for STOVL aircraft

Analysis of internal flow in a ventral nozzle for STOVL aircraft

By C. Frederic Smith

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

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

By Louis L Steers

View Modifications to the nozzle test chamber to extend nozzle static-test capability By J. Wayne Keyes

Modifications to the nozzle test chamber to extend nozzle static-test capability

Modifications to the nozzle test chamber to extend nozzle static-test capability

By J. Wayne Keyes

View René Leduc, pionnier de la propulsion à réaction By Jean Lacroze,Jean Lacrozze,Philippe Ricco
Cover of René Leduc, pionnier de la propulsion à réaction by jean lacroze,jean lacrozze,philippe ricco

René Leduc, pionnier de la propulsion à réaction

By Jean Lacroze,Jean Lacrozze,Philippe Ricco

View Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft By Barbara S. Esker

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

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

By Barbara S. Esker

View Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft By Barbara S. Esker

Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft

Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft

By Barbara S. Esker

View Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft By Barbara S. Esker

Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

By Barbara S. Esker

View Comparison of combustion efficiencies for ramjet engines By Jürgen W. Bergmann

Comparison of combustion efficiencies for ramjet engines

Comparison of combustion efficiencies for ramjet engines

By Jürgen W. Bergmann

View Hypersonic airbreathing propulsion By William H. Heiser
Cover of Hypersonic airbreathing propulsion by william h. heiser

Hypersonic airbreathing propulsion

By William H. Heiser

View Developments in high-speed-vehicle propusion systems By E. T. Curran
Cover of Developments in high-speed-vehicle propusion systems by e. t. curran

Developments in high-speed-vehicle propusion systems

By E. T. Curran

View Mach 10 experimental database of a three-dimensional scramjet inlet flow field By Scott D. Holland

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

By Scott D. Holland

View Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control By A. B Blair

Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

By A. B Blair

View Preliminary calibration of a generic scramjet combustor By P. A. Jacobs

Preliminary calibration of a generic scramjet combustor

Preliminary calibration of a generic scramjet combustor

By P. A. Jacobs

View Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi By Vladimir Isaakovich Polikovskiĭ

Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi

Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi

By Vladimir Isaakovich Polikovskiĭ

View Viscous flow simulations of internal store carriage and separation By Oktay Baysal

Viscous flow simulations of internal store carriage and separation

Viscous flow simulations of internal store carriage and separation

By Oktay Baysal

View High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics) By S. N. B. Murthy
Cover of High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics) by s. n. b. murthy

High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)

By S. N. B. Murthy