Transition Of The Laminar Boundary Layer On A Delta Wing With 74 Sweep In Free Flight At Mach Numbers From 2 8 To 5 3
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Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
language: en
Publisher:
Release Date: 1960-07
Technical Publications Announcements
Author: United States. National Aeronautics and Space Administration
language: en
Publisher:
Release Date: 1961