Trajectory Optimization of a Supersonic Aircraft with a Thermal Fuel Management System
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3884
Reference29 articles.
1. A Multidisciplinary Design Optimization Framework for Design Studies of an Efficient Supersonic Air Vehicle
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3. Infrared signature studies of aerospace vehicles
4. Fuel Thermal Management System Consideration in Conceptual Design Sizing
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