ADDITIONAL CALCULATIONS OF HYPERSONIC DYNAMIC STABILITY.
Quarterly status rept. no. 3, 29 May-28 Aug 64,
UNITED AIRCRAFT CORP EAST HARTFORD CONN
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Calculations of the hypersonic static and dynamic stability of ogive and ogive-cylinder fuselages, and of rectangular and delta wings in the presence of those fuselages, are presented. The results are compared with those calculated by Newtonian theory and by supersonic flow theories. A description is presented of wind tunnel models which are being constructed for tests to evaluate the predicted trends. Author