Accession Number : ADA019188

Title :   The Douglas Aerophysics Laboratory Four-Foot Trisonic Wind Tunnel,

Corporate Author : DOUGLAS AIRCRAFT CO INC HUNTINGTON BEACH CALIF MISSILE AND SPACE SYSTEMS DIV

Personal Author(s) : Raddatz,L. A.

Report Date : OCT 1967

Pagination or Media Count : 80

Abstract : This report describes the Four-Foot Trisonic Wind Tunnel and the Douglas Aerophysics Laboratory in which it is located. It also presents the performance and operating characteristics of the tunnel, model support and design considerations for a test, diverse test capabilities, instrumentation and data recording equipment, data processing and presentation, and the customer responsibilities for obtaining optimum planning and performance of wind tunnel tests.

Descriptors :   *Wind tunnels, *Variable area nozzles, Subsonic flow, Transonic flow, Supersonic flow, Performance, Operation, Model tests, Supports, Test methods, Test facilities, Instrumentation, Data acquisition, Data processing, Wind tunnel tests, Computer applications, Test equipment, Aerodynamic characteristics, Aerothermodynamics, Simulation, Movable nozzles

Subject Categories : Test Facilities, Equipment and Methods

Distribution Statement : APPROVED FOR PUBLIC RELEASE