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.
STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE ; 1968 ; PALM SPRINGS, CA, US
1968-04-01
Conference paper
No indication
English
Evaluation of aerothermoelasticity problems for unmanned Mars entry vehicles
Engineering Index Backfile | 1968
|Static Aerothermoelasticity of Hypersonic Vehicles
AIAA | 2017
|