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Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Three Aluminum-Alloy Models and One Steel Model of 20-Inch Chord and Span With Various Internal Structures and Skin Thicknesses
Author:
Rosecrans, Richard
Additional Authors:
Vosteen, Louis F.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57H01
Link:
https://digital.library.unt.edu/ark:/67531/metadc64327/
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