## Abstract When a reusable launch vehicle (RLV) returns to earth, it flies just by gliding without thrust. In this phase, one of the most likely and important faults to occur in the airframe is a jamming of the elevon. To tolerate this failure, the flight control system must keep stability and per
Flutter analysis for control surface of launch vehicle with dynamic stiffness
โ Scribed by Seung-Kil Paek; In Lee
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 619 KB
- Volume
- 60
- Category
- Article
- ISSN
- 0045-7949
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