Aerothermoelasticity problems for Mars entry vehicles, discussing deceleration loads, separated hot gas flow, shield thermal gradients and oscillatory body motion
Evaluation of aerothermoelasticity problems for unmanned Mars-entry vehicles.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN SOCIETY OF MECHANICAL ENGINEERS, STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE ; 1968 ; PALM SPRINGS, CALIF.
1969-02-01
Miscellaneous
No indication
English
Evaluation of aerothermoelasticity problems for unmanned Mars entry vehicles
Engineering Index Backfile | 1968
|Static Aerothermoelasticity of Hypersonic Vehicles
AIAA | 2017
|