Evaluating the dynamic response of in-flight thrust calculation techniques during throttle transients
- 20 June 1994
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Development of a real-time aeroperformance analysis technique for the X-29A advanced technology demonstratorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Use of the gas generator method to calculate the thrust of an afterburning turbofan enginePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971