Dynamic response of an axisymmetric thrust vector control nozzle
29th Aerospace Sciences Meeting ; 1991 ; Reno , NV , U.S.A.
1991-01-01
Conference paper
Electronic Resource
English
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method
BASE | 2021
|Two-dimensional thrust vector control nozzle
AIAA | 1991
|