Calculation of three-dimensional, inviscid supersonic, steady flows/

Main Author: Moretti, Gino
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center, Polytechnic Institute of New York
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982
Series:NASA contractor report NASA CR-3573
Subjects:
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100 1 |a Moretti, Gino 
245 1 0 |a Calculation of three-dimensional, inviscid supersonic, steady flows/  |c Gino Moretti ; prepared for Langley Research Center under grant NSG-1248 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration, Scientific and Technical Information Office,  |c 1982 
300 |a iii, 118 σ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA contractor report  |v NASA CR-3573 
500 |a "Polytechnic Institute of New York." 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Aerodynamics, Supersonic 
650 0 |a Airplanes  |x Fuselage 
650 0 |a Airframes 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Office 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Office 
710 2 |a Langley Research Center 
710 2 |a Polytechnic Institute of New York 
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