Accession Number : AD0606203
Title : ADDITIONAL CALCULATIONS OF HYPERSONIC DYNAMIC STABILITY.
Descriptive Note : Quarterly status rept. no. 3, 29 May-28 Aug 64,
Corporate Author : UNITED AIRCRAFT CORP EAST HARTFORD CONN
Personal Author(s) : Fink,Martin R.
Report Date : SEP 1964
Pagination or Media Count : 43
Abstract : 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)
Descriptors : (*AERODYNAMIC CONFIGURATIONS, STABILITY), (*HYPERSONIC FLOW, NUMERICAL ANALYSIS), WING BODY CONFIGURATIONS, RECTANGULAR BODIES, DELTA WINGS, CYLINDRICAL BODIES, SLENDER BODIES, OGIVES, FUSELAGES, DYNAMICS, BLUNT BODIES
Distribution Statement : APPROVED FOR PUBLIC RELEASE