Three-Dimensional Receptivity of a Blunt-Cone Boundary Layer to Incident Slow Acoustic Waves
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, 621000 Mianyang, People’s Republic of China
Funder
National Numerical Windtunnel
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061426
Reference45 articles.
1. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
2. The approximation properties determined by operator ideals
3. MorkovinM. V. “Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies,” U.S. Air Force Flight Dynamics Lab. AFFDL-TR 68–149, Wright Patterson Air Force Base, OH, 1969.
4. Boundary-Layer Stability and Transition
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