Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency
Author:
Funder
National Natural Science Foundation of China
Publisher
MDPI AG
Subject
General Physics and Astronomy
Link
http://www.mdpi.com/1099-4300/20/6/404/pdf
Reference39 articles.
1. Nosetip bluntness effects on transition at hypersonic speeds: experimental and numerical analysis under NATO STO AVT-240
2. Boundary-Layer Stability Analysis for Stetson’s Mach 6 Blunt-Cone Experiments
3. Analysis of Windward Side Hypersonic Boundary Layer Transition on Blunted Cones at Angle of Attack
4. Exploration of POD-Galerkin Techniques for Developing Reduced Order Models of Nonlinear Euler Equations
5. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
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1. Phenomenological Introduction of Standoff Distance of Sonic Ring Impelling Entropy Waves and Aerodynamic Heating of Hypersonic Vehicles;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27
2. Effect of three-dimensional smooth humps on hypersonic boundary layer instability of streamwise vortices over a yawed cone;Physics of Fluids;2021-06
3. Numerical Investigation on the Response Characteristics of Hypersonic Boundary Layer under Different Types of Finite Amplitude Pulse Disturbance Waves;Journal of Applied Fluid Mechanics;2021-01-01
4. Effect of a Roughness Element on the Hypersonic Boundary Layer Receptivity Due to Different Types of Free-Stream Disturbance with a Single Frequency;Entropy;2019-03-06
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