Wind tunnel testing of an axisymmetric isentropic relaxed external compression inlet at Mach 1.97 design speed

Keyphrases

• External Compression 100%
• Analytical Methodology 100%
• Experimental Database 100%
• Wind Tunnel Test 100%
• Isentropic 100%
• Design Speed 100%
• Mach number 50%
• Surface Treatment 50%
• System Performance 50%
• Bleeding 50%
• Diffuser 50%
• Design Work 50%
• Flow Properties 50%
• Model Design 50%
• Large Database 50%
• Mass Flow Rate 50%
• Aerospace 50%
• Flow Angle 50%
• Incoming Flow 50%
• Angle of Attack 50%
• Supersonic Wind Tunnel 50%
• Sonic Boom 50%
• Propulsion System 50%
• Flow Speed 50%
• Development Design 50%
• Inlet Design 50%
• Boundary Layer Control 50%
• Gulf Stream 50%
• Methodology Development 50%
• Test Planning 50%
• Treatment Concept 50%
• Struts Effect 50%
• Diffuser Length 50%
• Internal Flow Characteristics 50%

Engineering

• Axisymmetric 100%
• Isentropic 100%
• Design Speed 100%
• Significant Change 50%
• Flow Characteristics 50%
• Computational Fluid Dynamics 50%
• Boundary Layer 50%
• Systems Performance 50%
• Analytical Study 50%
• Design Method 50%
• Design Model 50%
• NASA 50%
• Subsonic Diffuser 50%
• Flow Property 50%
• Design Development 50%
• Mass Flowrate 50%
• Mach Number 50%
• Angle-of-Attack 50%
• Sonic Boom 50%
• Diffusers 50%
• Propulsion System 50%
• Internal Flow 50%
• Test Run 50%
• Wind Tunnel Test 50%
• Flow Speed 50%