NASA technical note

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Page 26 - Gaydon, AG, and Hurle, IR, The Shock Tube in High-Temperature Chemical Physics, Reinhold, New York, 1963.
Page 8 - A Review of Rate Constants of Selected Reactions of Interest In Re-Entry Flow Fields in the Atmosphere - MH Bortner (1969).* NBS Tech.
Page 20 - Raters lation 1 and 2 1 and 3 1 and 4 2 and 3 2 and 4 3 and 4...
Page 47 - DC 205^6 11. Contract or Grant No. 13. Type of Report and Period Covered 2. Sponsoring Agency Name and Address 14.
Page 25 - Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube With Hydrogen and Helium as Driver Gases.
Page 49 - RD and Morton, KW, Difference Methods for Initial -Value Problems.
Page 17 - No. 1, Feb. 1973, pp. 17-24. 4 Ludwig, Laurence P., "Face-Seal Lubrication. I — Proposed and Published Models," NASA TN D-8101, 1976. 5 Sneck, HJ, "The Effect of Geometry and Inertia on Face Seal Performance—Laminar Flow," JOURNAL OF LUBRICATION TECHNOLOGY, TRANS. ASME, Series F, Vol. 90. No.
Page 25 - A Preliminary Theoretical Study of the Expansion Tube, a New Device for Producing High-Enthalpy Short-Duration Hypersonic Gas Flows, NASA TR R-133 (1962) 54 VORREITER, JW and SHEPARD, Ch.

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