Accession Number : AD0766661

Title :   Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume III.

Descriptive Note : Technical rept.,

Corporate Author : CALSPAN CORP BUFFALO N Y

Personal Author(s) : DE Kuyper,R. E.

Report Date : JUL 1973

Pagination or Media Count : 666

Abstract : Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.

Descriptors :   (*GUIDED MISSILE MODELS, *TRANSONIC CHARACTERISTICS), WIND TUNNEL MODELS, CANARD CONFIGURATIONS, FINS, MODEL TESTS, THRUST, FORCE(MECHANICS), MOMENTS, STATISTICAL DATA

Subject Categories : Guided Missile Dynam, Config & Cntrl Surfaces
      Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE