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,
------------------------- --------------------- ------ --------- ------- ------- --------- --------
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,
------------------------- --------------------- ------ --------- ------- ------- --------- --------