Numerical Investigations on an Advanced Diverterless Supersonic Inlet with a Corner Bump in a Wing-Fuselage Installation (AIAA 2018-4746)
Joint propulsion conference
01.01.2018
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Design and optimization of bump (compression surface) for diverterless supersonic inlet
SAGE Publications | 2022
|