Low-speed wind-tunnel parametric investigation of various segments of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model/

Main Author: Croom, Delwin R.
Corporate Authors: United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1976
Series:NASA technical note D-8162
Subjects:
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245 1 0 |a Low-speed wind-tunnel parametric investigation of various segments of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model/  |c Delwin R. Croom ; Langley Research Center 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration, Scientific and Technical Information Office,  |c 1976 
300 |a 23 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical note  |v D-8162 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Spoilers (Airplanes)  |x Testing 
650 0 |a Airplanes  |x Models 
710 |a United States  |b National Aeronautics and Space Administration  |x Testing 
710 0 |a United States.  |b National Aeronautics and Space Administration 
710 2 |a Langley Research Center 
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