Hypersonic Fluid–Structure Interactions Due to Intermittent Turbulent Spots on a Slender Cone-Reference-Cited by-同舟云学术

Hypersonic Fluid–Structure Interactions Due to Intermittent Turbulent Spots on a Slender Cone

Published:2019-02 Issue:2 Volume:57 Page:749-759
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Casper Katya M.¹,Beresh Steven J.¹,Henfling John F.¹,Spillers Russell W.¹,Hunter Patrick¹,Spitzer Seth¹

Affiliation:

1. Sandia National Laboratories, Albuquerque, New Mexico 87185

Funder

National Nuclear Security Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057374

Reference35 articles.

1. Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone

2. PateS. R.BrownM. D. “Acoustic Measurements in Supersonic Transitional Boundary Layers,” Arnold Engineering Development Complex TR-69-182, Arnold AFB, TN, Oct. 1969.

3. Boundary layer acoustic measurements in transitional and turbulent flow at M infinity equals 4.0

4. An Experiment to Determine Nose Tip Transition with Fluctuating Pressure Measurements

5. Experimental Determination of the Aeroacoustic Environment about a Slender Cone

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