Accession Number : AD0676576

Title :   CALIBRATION MODELS FOR DYNAMIC STABILITY TESTS,

Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s) : Fail,R. ; Garner,H. C.

Report Date : 1968

Pagination or Media Count : 8

Abstract : This report describes three calibration models in the AGARD series. Model G: A slender wing. Suitable for tests over a wide speed range. Fitted with a fin and a sting fairing. Model H: A thin tapered wing suitable for high speed tests. Model J: A 10 degree semi-angle cone, suitable for high supersonic speed testing. (Author)

Descriptors :   (*DELTA WINGS, AERODYNAMIC CHARACTERISTICS), SLENDER BODIES, THIN WINGS, CONICAL BODIES, WIND TUNNEL MODELS, BOUNDARY LAYER TRANSITION, CALIBRATION, SUBSONIC CHARACTERISTICS, TRANSONIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS, STANDARDIZATION, WALLS, INTERFERENCE, FINS

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE