Accession Number : AD0298902

Title :   FAVORABLE WING-BODY INTERFERENCE FOR AIRCRAFT AT SUPERSONIC SPEED: AN ANALYTIC STUDY OF DESIGN PARAMETERS

Corporate Author : GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y

Personal Author(s) : MEYER,R.C.

Report Date : 08 SEP 1962

Pagination or Media Count : 1

Descriptors :   AERODYNAMIC CHARACTERISTICS, ASPECT RATIO, DRAG, EQUATIONS, INTERFERENCE, MATHEMATICAL ANALYSIS, MATHEMATICAL PREDICTION, SUPERSONIC CHARACTERISTICS, TABLES(DATA)

Distribution Statement : APPROVED FOR PUBLIC RELEASE