Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee/

Main Author: Sleeman, William C.
Corporate Authors: United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors: Forsyth, David R.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, 1977
Series:NASA technical note 8488
Subjects:
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245 1 0 |a Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee/  |c William C. Sleeman, Jr. and David R. Forsyth 
260 |a Washington:  |b National Aeronautics and Space Administration,  |c 1977 
300 |a 77 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical note  |v 8488 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Lift (Aerodynamics) 
650 0 |a Jet flaps (Airplanes) 
700 1 |a Forsyth, David R. 
710 |a United States  |b National Aeronautics and Space Administration 
710 0 |a United States.  |b National Aeronautics and Space Administration 
710 2 |a Langley Research Center 
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