Energy-state approximation in performance optimization of supersonicaircraft
- 1 November 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (6) , 481-488
- https://doi.org/10.2514/3.44093
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Steepest-Ascent Method for Solving Optimum Programming ProblemsJournal of Applied Mechanics, 1962
- Energy Approach to the General Aircraft Performance ProblemJournal of the Aeronautical Sciences, 1954