Large-Eddy Simulations of the Unsteady Behavior of a Hypersonic Intake at Mach 5-Reference-Cited by-同舟云学术

Large-Eddy Simulations of the Unsteady Behavior of a Hypersonic Intake at Mach 5

Published:2021-10 Issue:10 Volume:59 Page:3859-3872
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

De Vanna Francesco¹,Picano Francesco¹,Benini Ernesto¹,Quinn Mark Kenneth²

Affiliation:

1. University of Padova, 35131 Padova, Italy

2. The University of Manchester, Manchester, England M1 3NJ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060160

Reference42 articles.

1. FerriA.NucciL. M.FieldL. “The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions,” National Advisory Committee for Aeronautics, Research Memorandum, 1951.

2. Supersonic Diffuser Instability

3. FisherB. S. A.NealeM. C.BrooksA. J. “On the Sub-Critical Stability of Variable Ramp Intakes at Mach Numbers Around 2,” Ministry of Defence (Procurement Executive), Aeronautical Research Council Reports and Memoranda, 1972, https://reports.aerade.cranfield.ac.uk/handle/1826.2/2987.

4. Experimental Study of Supersonic Inlet Buzz

5. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

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