Results of a thermal/structural design analysis study of a fuel injection strut for an airframe integrated hydrogen cooled scramjet are presented. It is indicated that a feasible thermal/structural concept has been identified for the static load conditions and that thermal stresses dominate the response. It is suggested that the response of the concept to dynamic loads be investigated.
Thermostructural analysis of a scramjet fuel-injection strut
1978-01-01
Conference paper
No indication
English
Advanced Carbon/Carbon Injection Strut for Actual Scramjet
British Library Conference Proceedings | 1996
|A hydrogen cooled injection strut design for scramjet
AIAA | 1996
|A Hydrogen Cooled Injection Strut Design for Scramjet
British Library Conference Proceedings | 1996
|