Boundary Layers on a Flat Plate at Sub- and Superorbital Speeds

Author:

Hayne Michael J.1,Mee David J.1,Gai Sudhir L.2,McIntyre Timothy J.1

Affiliation:

1. The University of Queensland, Brisbane, Queensland 4072, Australia

2. University of New South Wales, Australian Defence Force Academy, Canberra, Australian Capital Territory 2600, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Reference32 articles.

1. Neely, A. J. "Experimental and Analytical Study of a Pilot Superorbital Expansion Tube for Aerothermodynamic Testing to 13 km=s in Air," Ph.D. Thesis,Department of Mechanical Engineering, Univ. of Queensland, Brisbane, Australia,1996.

2. Measurements of heat transfer to a flat plate in a dissociated high-enthalpy laminar air flow

3. Doolan, C. J. "A Two-Stage Free Piston Driver for Hypervelocity Expansion Tubes," Ph.D. Thesis,Department of Mechanical Engineering, Univ. of Queensland, Brisbane, Australia,1996.

4. Free-Piston Driven Expansion Tubes

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