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Aerodynamic design integration of supersonic aircraft
Home
Publications
Aerodynamic design integration of supersonic aircraft
Aerodynamic design integration of supersonic aircraft
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D. Baals
D. Baals
JH
Jr. R. Harris
Jr. R. Harris
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16 August 1968
proceedings article
Published by
American Institute of Aeronautics and Astronautics (AIAA)
https://doi.org/10.2514/6.1968-1018
Abstract
No abstract available
Cited by 9 articles