Accession Number : ADA950045

Title :   Investigation of Free-Stream Pressure and Stagnation Pressure Measurement from Transonic and Supersonic Aircraft. II. Experimental.

Descriptive Note : Interim phase rept.,

Corporate Author : UNIVERSITY OF SOUTHERN CALIFORNIA LOS ANGELES ENGINEERING CENTER

Personal Author(s) : Mannes, Robert L. ; Stuart, Jay W., Jr

Report Date : JUL 1956

Pagination or Media Count : 132

Descriptors :   *PRESSURE MEASUREMENT, *PITOT TUBES, TRANSONIC FLOW, SUPERSONIC FLOW, ANGLE OF ATTACK, SIDESLIP, STAGNATION PRESSURE, FREE STREAM, PRESSURE, COMPENSATION, BASE PRESSURE, VARIATIONS, ERRORS, PROBES.

Subject Categories : Test Facilities, Equipment and Methods
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE