Accession Number : AD0342159

Title :   DEVELOPMENT, ANALYSIS, AND TESTING OF CANTILEVERED 6%-THICK 70 DEGREES DELTA WING FLUTTER MODELS, PART I. SUPERSONIC TESTS.

Descriptive Note : Rept. for Jun 60-Feb 63,

Corporate Author : AEROJET-GENERAL CORP AZUSA CA

Personal Author(s) : Mazelsky, Bernard ; Amey, Harry B., Jr. ; Cunningham, Patrick J.

Report Date : AUG 1963

Pagination or Media Count : 48

Descriptors :   (*DELTA WINGS, FLUTTER), WIUND TUNNEL MODELS, MODEL TESTS, SUPERSONIC CHARACTERISTICS, HYPERSONIC CHARACTERISTICS.

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE