1-24 of 81 Books
Turbofan forced mixer-nozzle internal flowfield
Turbofan forced mixer-nozzle internal flowfield
By Robert W. Paterson
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
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
Control of aircraft and missile powerplants
Control of aircraft and missile powerplants
By Albert J. Sobey
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
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
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
Virtualʹnye aviadvigateli
Virtualʹnye aviadvigateli
By A. N. Zhukov
Comparison of combustion efficiencies for ramjet engines
Comparison of combustion efficiencies for ramjet engines
By Jürgen W. Bergmann

Hypersonic airbreathing propulsion
By William H. Heiser

Developments in high-speed-vehicle propusion systems
By E. T. Curran
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
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
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

René Leduc, pionnier de la propulsion à réaction
By Jean Lacroze,Jean Lacrozze,Philippe Ricco
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
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
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
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
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
Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi
Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi
By Vladimir Isaakovich Polikovskiĭ

High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)
By S. N. B. Murthy
A parametric study of a gas-generator airturbo ramjet (ATR)
A parametric study of a gas-generator airturbo ramjet (ATR)
By Christopher Snyder
Contribution à l'etude aérodynamique du statoréacteur subsonique
Contribution à l'etude aérodynamique du statoréacteur subsonique
By O. Schrenk