Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surface

By A. Rasheed, H. Hornung, A. Fedorov, Norman D. Malmuth. 2002

216 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/3901ab71f7e3c37bd4f4062abcbe87e819bdaf1e

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. A. Fedorov

In Applied Mathematics

1. A. Fedorov
2. Norman D. Malmuth

In Computational Mechanics

1. A. Fedorov
2. Norman D. Malmuth
3. X. Zhong
4. Xiaowen Wang
5. Yanbao Ma

Citations in the corpus

• Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating (2003, methodology): “Stabilization of a hypersonic boundary layer 101 California Institute of Technology GALCIT T-5 shock tunnel (Rasheed et al. 2002) by testing a 5◦ half-angle sharp cone. The cone in these tests had one half of its surface solid and the other a porous sheet that was perforated with equally spaced blin”