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Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Two Aluminum-Alloy Models of 20-Inch Chord With 0.064- and 0.081-Inch-Thick Skin
Author:
Griffith, George E.
Additional Authors:
Miltonberger, Georgene H.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55F13
Link:
https://digital.library.unt.edu/ark:/67531/metadc61471/
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