NASA / TN D-1380
Young,Lou S
EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0 / .- Nasa, Washington, D.C., 1962 .- 23 .
Bound With Nasa Tn D-1376-79
Copy Details:
Acc. No.: TR12901, Full Call No.: NASA TN D-1380, Item type: Technical Report , Location: General Stacks,
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Young,Lou S
EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0 / .- Nasa, Washington, D.C., 1962 .- 23 .
Bound With Nasa Tn D-1376-79
Copy Details:
Acc. No.: TR12901, Full Call No.: NASA TN D-1380, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------