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Maslach, G. J.; Schaaf, S. A.

Cylinder drag in the transition from continuum to free-molecule flow. (English) Zbl 0112.19201

Phys. Fluids 6, 315-321 (1963).
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Cited in 10 Documents

Keywords:

fluid mechanics
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References:

[1] S. A. Schaaf, ”Mechanics of Rarefied Gases,” inHandbuch der Physik, edited by S. Flügge (Springer-Verlag, Berlin, 1963), Vol. VIII.
[2] Millikan, Phys. Rev. 22 pp 1– (1923)
[3] D. J. Masson, D. N. Morris, and D. E. Bloxsom, ”Measurements of Sphere Drag from Hypersonic Continuum to Free Molecular Flow,” inRarefied Gas Dynamics(Academic Press, Inc., New York, 1961), pp. 643–662.
[4] J. R. Stalder, G. Goodwin, and M. O. Creager, NACA, TN-2438 (1951).
[5] F. S. Sherman, NACA, TN-3298 (1955).
[6] Laurmann, Phys. Fluids 1 pp 469– (1958)
[7] C. F. Dewey, ”Hot Wire Measurements in Low Reynolds Number Hypersonic Flows,” Guggenheim Aeronautical Laboratory, California Institute of Technology, Memo No. 63 (1961).
[8] G. J. Maslach and F. S. Sherman, ”Design and Testing of an Axi-Symmetric Hypersonic Nozzle for a Low Density Wind Tunnel,” Wright Air Development Center Tech. Rept. TR-341 (1956).
[9] D. E. Emerson and S. A. Schaaf, ”Performance of a Supersonic Nozzle in the Rarefied Gas Dynamics Regime,” University of California Engineering Project Rept. HE-150-72 (1950).
[10] J. M. Owen and F. S. Sherman, ”Design and Testing of a Mach 4 Axially Symmetric Nozzle for Rarefied Gas Flows,” University of California Engineering Project Rept. HE-150-104 (1952).
[11] G. J. Maslach and R. N. Latz, ”Force Measurements in Low Density Hypersonic Air Flows,” inAdvances in Vacuum Science and TechnologyPergamon Press, New York, 1960), Vol. II, pp. 809–812.
[12] J. Aroesty, ”Sphere Drag in a Low Density Supersonic Flow,” Ph.D. thesis, University of California (1962).
[13] H. N. Riise, ”Compressible Flow Tables for Air in Increments of 0.001 in Mach Number,” Jet Propulsion Laboratory, Publ. No. 27 (1954).
[14] Bromley, Ind. Eng. Chem. 43 pp 1641– (1951)
[15] A. Sreekanth, ”Drag Measurements in Circular Cylinders and Spheres in the Transition Region at a Mach Number of 2,” University of Toronto UTIA Rept. 74 (1961).
[16] G. J. Maslach and L. Talbot, ”Low Density Aerodynamic Characteristics of a Cone at Angle of Attack,” University of California Engineering Project Rept. HE-150-172 (1959).
[17] Schaaf, ARS J. 31 pp 194– (1961) · Zbl 0098.17105 · doi:10.2514/8.5424
[18] F. E. Gowen and E. W. Perkins, NACA TN-2960 (1953).
[19] S. A. Schaaf, ”Aerodynamics of Satellites,” Rand Company Rept. R-339 (1959), Sec. 1.
[20] Lunc, Arch. Mech. Stos. 8 pp 597– (1956)
[21] Lunc, Bull. de l’Acad. Pol. des Sci. 5 pp 47– (1956)
[22] Baker, Phys. Fluids 1 pp 73– (1958)
[23] D. R. Willis, Ph.D. thesis, Princeton University (1959).
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