TY  - BOOK
AU  - Stokes, Fred H. 
AU  - Matthews, J. T.
TI  - Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
U1  - NACA 
PY  - 1953///
CY  - Washington, D. C. 
PB  - National Advisory Committee for Aeronautics
ER  -