Receptivity of Boundary Layer over a Blunt Wedge due to Freestream Pulse Disturbances at Mach 6
Author:
Affiliation:
1. College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China
2. Beijing Spacecrafts, China Academy of Space Technology, Beijing 100094, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
Hindawi Limited
Subject
Aerospace Engineering
Link
http://downloads.hindawi.com/journals/ijae/2016/3196057.pdf
Reference34 articles.
1. An experimental investigation of flow and heat transfer characteristics over blocked surfaces in laminar and turbulent flows
2. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
3. Existence and Stability of Noncharacteristic Boundary Layers for the Compressible Navier–Stokes and Viscous MHD Equations
4. The effects of variable specific heat on the stability of hypersonic boundary layer on a flat plate
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