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West, F. E.
       Effects of body-mounted lateral controls and speed brakers the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.90. [NASA TN D-522] / .- NASA: Washington, D.C., 1960 .- various pagings.
Bound With NASA TN D-521,523-530.
Copy Details:
Acc. No.: TR15667, Full Call No.: NASA TN D-522, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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