Cover Image

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Bibliographic Details
Main Author: Reubush, David E.
Corporate Authors: Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington : U.S. National Aeronautics and Space Administration ; 1976.
Series:NASA technical note ; NASA TN D-8238.
Subjects:
Drag (Aerodynamics)
Reynolds number.

Evans: US Documents (Annex 5th floor)

Holdings details from Evans: US Documents (Annex 5th floor)
Call Number: NAS 1.14:D-8238
 
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NAS 1.14:D-8238 Available