Analysis of shock oscillations of an external compression supersonic inlet through unsteady numerical simulations-Reference-Cited by-同舟云学术

Analysis of shock oscillations of an external compression supersonic inlet through unsteady numerical simulations

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 Applied Aerodynamics Conference
language:
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Author:

Grenson Pierre¹,Beneddine Samir¹

Affiliation:

1. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3011

Reference22 articles.

1. Ferri, A., and Nucci, L. M. “The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions,” Tech. Rep. NACA RM-L50K30, 1951.

2. Supersonic Diffuser Instability

3. Fisher, S., Neale, M., and Brooks, A. “On the sub-critical stability of variable ramp intakes at mach numbers around 2,” Tech. Rep. ARC-R/M-3711, National Gas Turbine Establishment, 1970.

4. Experimental Study of Supersonic Inlet Buzz

5. Numerical Simulation of Near-Critical and Unsteady, Subcritical Inlet Flow

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