Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution Page: 3 of 94
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NACA EM A56105
TABLE OF CONTENTS - Concluded
APPENDIX B - RELATIVE CONTRIBUTIONS OF AERODYNAMIC DAMPING
AND DAMPING DUE TO DYNAMIC-PRESSURE VARIATION . . . . . . . 45
APPENDIX C - METHOD OF CALCULATING BOUNDARY-IAYER THICKNESS . . . . 50
REFERENCES ... .. . . .. * 4 52
FIGURES. .......................... . 57
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Seiff, Alvin; Sommer, Simon C. & Canning, Thomas N. Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution, report, January 14, 1957; (digital.library.unt.edu/ark:/67531/metadc64511/m1/3/: accessed October 18, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.