Normal-Shock/Boundary-Layer Interactions in Transonic Intakes at High Incidence-Reference-Cited by-同舟云学术

Normal-Shock/Boundary-Layer Interactions in Transonic Intakes at High Incidence

Published:2019-07 Issue:7 Volume:57 Page:2867-2880
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Coschignano A.,Babinsky H.,Sheaf C.,Zamboni G.

Funder

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J058054

Reference26 articles.

1. MillerB. A.DastoliB. J. “Effect of Entry Lip Design on Aerodynamics and Acoustics of High-Throat- Mach-Number Inlets for the Quiet, Clean, Short-Haul Experimental Engine,” NASA TP 3222, 1975.

2. Internal cowl-separation at high incidence angles

3. AlbersJ. A.MillerB. A. “Effect of Subsonic Inlet Lip Geometry on Predicted Surface and Flow Mach Number Distributions,” NASA TN 7446, 1973.

4. Prediction of Boundary-Layer Flow Separation in V/STOL Engine Inlets

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