Accession Number : AD0759708

Title :   Force and Pressure Tests of a Six Caret-Wing-Body Model,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Mruk,G. K.

Report Date : 20 FEB 1968

Pagination or Media Count : 189

Abstract : Tests to determine six-component force and pressure distribution data on a six caret-wing-body model were performaned in a hypersonic shock tunnel. The report presents the details of the test program, a description of the model and equipment used, and a tabular and graphic presentation of obtained data.

Descriptors :   (*WING BODY CONFIGURATIONS, AERODYNAMIC LOADING), GEOMETRIC FORMS, AERODYNAMIC CHARACTERISTICS, SHOCK TUBES, TEST EQUIPMENT, PITCH(MOTION), YAW, ENTHALPY

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE