Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions-Reference-Cited by-同舟云学术

Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions

Published:2021-07 Issue:7 Volume:59 Page:2737-2752
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Brouwer Kirk R.¹,Perez Ricardo A.²,Beberniss Timothy J.²,Spottswood S. Michael²,Ehrhardt David A.³

Affiliation:

1. ARCTOS Technology Solutions, Beavercreek, Ohio 45432

2. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

3. University of Illinois at Urbana-Champaign, Champaign, IL 61820

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060114

Reference45 articles.

1. ZuchowskiB. “Predictive Capability for Hypersonic Structural Response and Life Prediction, Phase I—Identification of Knowledge Gaps,” AFRL-RB-WP-TR-2010-3069, Wright–Patterson AFB, OH, 2010.

2. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future

3. DixonS. C.GriffithG. E.BohonH. L. “Experimental Investigation at Mach Number 3.0 of the Effects of Thermal Stress and Buckling on the Flutter of Four-Bay Aluminum Alloy Panels with Length-Width Ratios of 10,” NASA TN D-921, 1961.

4. DixonS. C. “Experimental Investigation at Mach Number 3.0 of Effects of Thermal Stress and Buckling on Flutter Characteristics of Flat Single-Bay Panels of Length-Width Ratio 0.96,” NASA TN D-1485, 1962.

5. DixonS. C.ShoreC. P. “Effects of Differential Pressure, Thermal Stress and Buckling on Flutter of Flat Panels with Length-Width Ratio of 2,” NASA TN D-2047, 1963.

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