Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment-Reference-Cited by-同舟云学术

Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment

Published:2020-10 Issue:10 Volume:58 Page:4322-4338
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Masini Luke¹,Timme Sebastian¹,Peace Andrew J.²

Affiliation:

1. University of Liverpool, Liverpool, England L69 3GH, United Kingdom

2. Aircraft Research Association, Ltd., Bedford, England MK41 7PF, United Kingdom

Funder

UK Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference62 articles.

1. HiltonW. F.FowlerR. G. “Photographs of Shock Wave Movement,” National Physical Lab. R&M 2692, United Kingdom, 1947.

2. McDevittJ. B.OkunoA. F. “Static and Dynamic Pressure Measurements on a NACA 0012 Airfoil in the Ames High Reynolds Number Facility,” NASA TP 2485, Jun. 1985.

3. Experimental Study of Shock Oscillation over a Transonic Supercritical Profile

4. BrunetV. “Computational Study of Buffet Phenomenon with Unsteady RANS Equations,” AIAA Paper 2003-2679, 2003.

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