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
Distribution Statement : APPROVED FOR PUBLIC RELEASE