The Free Molecule Probe and Its Use for the Study of Leading Edge Flows

Author:

Laurmann J. A.

Publisher

AIP Publishing

Subject

General Engineering

Reference20 articles.

1. L. Talbot, “Viscosity corrections to cone probes in rarefied supersonic flow at a nominal Mach number of 4,” NACA TN 3219 (1954).

2. Talbot, Koga, and Sherman, “Hypersonic viscous flow over slender cones,” University of California Engineering Project Report HE-150-147 (1957).

3. Stalder, Goodwin, and Creager, “A comparison of theory and experiment for high-speed free molecule flow,” NACA Report 1032 (1951).

4. Heat Transfer to a Cylinder for the Free Molecule Flow of a Nonuniform Gas

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1. Hot wire anemometry in rarefied gas flow;Journal of Physics E: Scientific Instruments;1980-09

2. Hot wire anemometry in low density flows;Propulsion and ASW Meeting;1970-05-04

3. Kinetic Theory of the Sharp Leading Edge Problem in Supersonic Flow;Physics of Fluids;1969

4. Hypersonic viscous flow over slender bodies with sharp leading edges.;AIAA Journal;1968-10

5. Hypersonic viscous flow over slender bodies with sharp leading edges;6th Aerospace Sciences Meeting;1968-01-22

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