Can Thrust Vectoring Save a Doomed Transport Jet?

L. Qian,; B.Gal-Or,; E. Kreindler,

doi:10.1515/TJJ.1998.15.2.89

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Can Thrust Vectoring Save a Doomed Transport Jet?

L. Qian, , B.Gal-Or, and E. Kreindler,

Published/Copyright: June 1, 1998

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From the journal International Journal of Turbo and Jet Engines Volume 15 Issue 2

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Harvard
Chicago
Vancouver

Qian,, L., B.Gal-Or,, and Kreindler,, E.. "Can Thrust Vectoring Save a Doomed Transport Jet?" International Journal of Turbo and Jet Engines, vol. 15, no. 2, pp. 89-90. https://doi.org/10.1515/TJJ.1998.15.2.89

Qian,, L., B.Gal-Or, & Kreindler,, E. (). Can Thrust Vectoring Save a Doomed Transport Jet?. International Journal of Turbo and Jet Engines, 15(2), 89-90. https://doi.org/10.1515/TJJ.1998.15.2.89

Qian,, L., B.Gal-Or,. and Kreindler,, E. () Can Thrust Vectoring Save a Doomed Transport Jet?. International Journal of Turbo and Jet Engines, Vol. 15 (Issue 2), pp. 89-90. https://doi.org/10.1515/TJJ.1998.15.2.89

Qian,, L., B.Gal-Or,, and Kreindler,, E.. "Can Thrust Vectoring Save a Doomed Transport Jet?" International Journal of Turbo and Jet Engines 15, no. 2 (): 89-90. https://doi.org/10.1515/TJJ.1998.15.2.89

Qian, L, B.Gal-Or,, Kreindler, E. Can Thrust Vectoring Save a Doomed Transport Jet?. International Journal of Turbo and Jet Engines. ;15(2): 89-90. https://doi.org/10.1515/TJJ.1998.15.2.89

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Published Online: 1998-06

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Articles in the same Issue

CONTENTS
Can Thrust Vectoring Save a Doomed Transport Jet?
Jet Deflection Angles in Military, Civil and RPV Thrust Vectoring Aircraft
A Family of Variational Principles for Compressible Rotational Blade-to-Blade Flow Using Semi-Inverse Method
Generalized Variational Principle for Compressible S2-Flow in Mixed-Flow Turbomachinery Using Semi-Inverse Method
Inviscid-Viscous Iterative Solution for Flowfield in Transonic Compressor Rotor
Turbine Performance Increases Through Airfoil Clocking
Ignition Behaviors of Fuel Droplets in a Hot Convective Flowfield
Effect of Dump Gap on Velocity Distribution and Flow Split in a Prototype Reverse-Flow Gas Turbine Combustor

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https://doi.org/10.1515/TJJ.1998.15.2.89

Articles in the same Issue

CONTENTS
Can Thrust Vectoring Save a Doomed Transport Jet?
Jet Deflection Angles in Military, Civil and RPV Thrust Vectoring Aircraft
A Family of Variational Principles for Compressible Rotational Blade-to-Blade Flow Using Semi-Inverse Method
Generalized Variational Principle for Compressible S2-Flow in Mixed-Flow Turbomachinery Using Semi-Inverse Method
Inviscid-Viscous Iterative Solution for Flowfield in Transonic Compressor Rotor
Turbine Performance Increases Through Airfoil Clocking
Ignition Behaviors of Fuel Droplets in a Hot Convective Flowfield
Effect of Dump Gap on Velocity Distribution and Flow Split in a Prototype Reverse-Flow Gas Turbine Combustor