Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /
David E. Reubush ; Langley Research Center, Hampton, Va.
APA Citation
Reubush, D. E., United States. National Aeronautics and Space Administration., Langley Research Center. (1976). Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations. Washington: U.S. National Aeronautics and Space Administration .
MLA Citation
Reubush, David E, United States. National Aeronautics and Space Administration, and Langley Research Center. Effect of Reynolds Number On the Subsonic Boattail Drag of Several Wing-body Configurations. Washington: U.S. National Aeronautics and Space Administration , 1976.
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