Steady subsonic flow around finite-thickness wings/

Main Author: Kuo, Ching-Chiang
Corporate Authors: United States National Aeronautics and Space Administration, Boston University, Langley Research Center
Other Authors: Morino, L.
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, 1975
Series:NASA contractor report NASA CR-2616
Subjects:
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100 1 |a Kuo, Ching-Chiang 
245 1 0 |a Steady subsonic flow around finite-thickness wings/  |c Ching-Chiang Kuo and Luigi Morino 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration,  |c 1975 
300 |a 79 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA contractor report  |v NASA CR-2616 
500 |a "Prepared by Boston University for Langley Research Center" 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
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650 0 |a Unsteady flow (Aerodynamics)  |x Mathematical models 
650 0 |a Aerodynamics  |x Mathematical models 
650 0 |a Airplanes  |x Wings 
700 1 |a Morino, L.  |x Mathematical models 
710 |a United States  |b National Aeronautics and Space Administration 
710 2 |a Boston University 
710 0 |a Langley Research Center 
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