Accession Number : AD0274625

Title :   SUPERSONIC WIND TUNNEL TESTS ON EXPERIMENTAL STATIC PRESSURE PROBES

Corporate Author : UNIVERSITY OF SOUTHERN CALIFORNIA LOS ANGELES ENGINEERING CENTER

Personal Author(s) : REHM,WALTER P.

Report Date : 31 JAN 1962

Pagination or Media Count : 1

Descriptors :   *FLIGHT INSTRUMENTS, *PITOT TUBES, AERODYNAMIC CHARACTERISTICS, MEASUREMENT, MODEL TESTS, PRESSURE, SUPERSONIC FLOW, WIND TUNNEL MODELS

Distribution Statement : APPROVED FOR PUBLIC RELEASE