Numerical Investigations on an Advanced Diverterless Supersonic Inlet with a Corner Bump in a Wing-Fuselage Installation
2018 Joint Propulsion Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2018
|Design and optimization of bump (compression surface) for diverterless supersonic inlet
SAGE Publications | 2022
|