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Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on a medium range wide-body tri-jet airplane model

By Croom, D. R.

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Book Id: WPLBN0002204576
Format Type: PDF eBook :
File Size: 4.2 MB
Reproduction Date: 2012
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Title: Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on a medium range wide-body tri-jet airplane model  
Author: Croom, D. R.
Volume:
Language: English
Subject: AEROSPACE ENGINEERING, STRESSES, SPACE ERECTABLE STRUCTURES
Collections: NASA Publication Collection
Historic
Publication Date:
1976
Publisher:

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R, C. D., M, W. G., & D, V. R. (1976). Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on a medium range wide-body tri-jet airplane model. Retrieved from http://www.netlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; An investigation was made in the V/STOL tunnel to determine, by the trailing wing sensor technique, the effectiveness of various segments of

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: AEROSPACE ENGINEERING; STRESSES; SPACE ERECTABLE STRUCTURES; MANUALS; STRUCTURAL STABILITY; TENSILE STRENGTH; STRUCTURAL ENGINEERING; COMPOSITE MATERIALS; FRACTURE MECHANICS; LOADS (FORCES); PLATES (STRUCTURAL MEMBERS); SHELLS (STRUCTURAL FORMS)

 

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