AERODYNAMIC DESIGN OPTIMIZATION OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING
International Council of the Aeronautical Sciences
2021-01-01
20 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Propulsion over a Wide Mach Number Range
NTIS | 1989
|Propulsion over a wide Mach number range
NTRS | 1989
|