Accession Number : AD0769059
Title : A Method for Determining the Pressure on the Surface of a Model during Aerodynamic Testing,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Maikapar,G. I. ; Khalezov,D. V.
Report Date : 18 OCT 1973
Pagination or Media Count : 5
Abstract : In experimental aerodynamics the familiar method of pressure determination limits the test capabilities due to the need for positioning a large number of sensors on the model. The present method obtains a continuous pressure distribution on models having complex shapes by coating a nonheat-conducting model with two heat-indicating coatings having different time dependent critical temperatures.
Descriptors : (*WIND TUNNEL MODELS, *TEST EQUIPMENT), (*AERODYNAMICS, *PATENTS), TEMPERATURE, PRESSURE, COATINGS, HEAT TRANSFER, TIME, MOTION PICTURE PHOTOGRAPHY, USSR
Subject Categories : Test Facilities, Equipment and Methods
Distribution Statement : APPROVED FOR PUBLIC RELEASE