Design of a Modular Boundary Layer Bleed System for a Supersonic Wind Tunnel
AIAA Aviation 2019 Forum
01.01.2019
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2019-3602: Design of a Modular Boundary Layer Bleed System for a Supersonic Wind Tunnel
British Library Conference Proceedings | 2019
|Supersonic-inlet boundary-layer bleed flow
AIAA | 1996
|Supersonic-lnlet Boundary-Layer Bleed Flow
Online Contents | 1996
|Modeling Supersonic Inlet Boundary-Layer Bleed Roughness
Online Contents | 1993
|Passive Boundary-Layer Bleed for Supersonic Intakes
British Library Online Contents | 1992
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