Supersonic Boundary-Layer Combustion via Multiporthole Injector Arrays

Author:

Pudsey Adrian S.1,Wheatley Vincent2,Boyce Russell R.3

Affiliation:

1. Institute for Thermodynamics, University of the Federal Armed Forces Munich, 85577 Neubiberg, Germany

2. School of Mechanical and Mining Engineering, The University of Queensland, Brisbane, Queensland 4072, Australia

3. The University of New South Wales, Canberra, Australian Capital Territory 2600, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference31 articles.

1. AIRCRAFT LAMINAR FLOW CONTROL

2. Current status of the use of wall compliance for laminar-flow control

3. Turbulent drag reduction using compliant surfaces

4. HwangD. P. “Skin Friction Reduction by Micro-Blowing Technique,” U.S. Patent No. 5,803,410, Sept. 1998.

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