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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