NACA / TM-1420
Corcos,G M
ON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE
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.- National Advisory Committee For Aeronautics, Washington,D.C., 1956
.- 43 .
Bound With Naca Tm-1421-1429.
Author Added Entry:
Liepmann,H W;
Copy Details:
Acc. No.: 17288, Full Call No.: NACA TM-1420, Item type: Technical Report , Location: General Stacks,
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