Design and optimization of bump (compression surface) for diverterless supersonic inlet
In this article design and optimization scheme of a three-dimensional bump surface for a
supersonic aircraft is presented. A baseline bump and inlet duct with forward cowl lip is …
supersonic aircraft is presented. A baseline bump and inlet duct with forward cowl lip is …
[PDF][PDF] CONEM2024-0784 ANGLE OF ATTACK EFFECTS ON THE PERFORMANCE OF A DIVERTERLESS SUPERSONIC INLET
JJ Vaca-Rios, J Oliveira, H Cerón-Muñoz - researchgate.net
The numerical simulations of a forebody with a Diverterless Supersonic Inlet (DSI) in three
dimensions have been studied. A type of external supersonic flow compression known as a …
dimensions have been studied. A type of external supersonic flow compression known as a …
[PDF][PDF] COB-2023-0382 PRELIMINARY AERODYNAMICS ANALYSIS OF A THREE-DIMENSIONAL BUMP AT SUBSONIC AND SUPERSONIC FLOW
JJ Vaca-Rios, H Cerón-Muñoz - researchgate.net
A three-dimensional compression surface (bump) is used in the inlet system of an aircraft
engine to compress the incoming airflow and reduce the boundary layer that is built up over …
engine to compress the incoming airflow and reduce the boundary layer that is built up over …