NACA / TN-2882
Stokes, Fred H.
Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
/ Fred, H. Stokes and J. T. Matthews
.- Washington, D. C. : National Advisory Committee for Aeronautics, 1953
.- 41p.
Author Added Entry:
Matthews, J. T.;
Copy Details:
Acc. No.: 67708B, Full Call No.: NACA TN-2882, Item type: Technical Report , Location: Reference,
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