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In-flight flow visualization results from the X-29A aircraft at high angles of attack

By Delfrate, John H.

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Book Id: WPLBN0002209383
Format Type: PDF eBook :
File Size: 1.7 MB
Reproduction Date: 2012

Title: In-flight flow visualization results from the X-29A aircraft at high angles of attack  
Author: Delfrate, John H.
Volume:
Language: English
Subject: ADVANCED LAUNCH SYSTEM (STS), OPERATING COSTS, PROPULSION SYSTEM CONFIGURATIONS
Collections: NASA Publication Collection
Historic
Publication Date:
1992
Publisher:

Citation

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H, D. J., & A, S. J. (1992). In-flight flow visualization results from the X-29A aircraft at high angles of attack. Retrieved from http://worldlibrary.in/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Flow visualization techniques were used on the X-29A aircraft at high angles of attack to study the vortical flow off the forebody and the s

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: ADVANCED LAUNCH SYSTEM (STS); OPERATING COSTS; PROPULSION SYSTEM CONFIGURATIONS; OXYGEN-HYDROCARBON ROCKET ENGINES; BOOSTER ROCKET ENGINES; EXPENDABLE STAGES (SPACECRAFT); REUSABLE ROCKET ENGINES; ROCKET ENGINE DESIGN; SPACE TRANSPORTATION SYSTEM; LOW COST

 

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