Precision flow-direction/pitot-static pressure probes, ranging from 0.035 to 0.090 inch (0.89 to 2.29 mm) in outside diameter, successfully fabricated and calibrated for use in Langley 20-inch Mach 6 Tunnel. Probes simultaneously measure flow direction and static and pitot pressures in flow fields about configurations in hypersonic flow at temperatures up to 500 degree F (260 degree C).
Miniature Flow-Direction/Pitot-Static Pressure Probes
NASA Tech Briefs ; 13 , 3
1989-03-01
Sonstige
Keine Angabe
Englisch
Minimum Performance Standard for Pitot and Pitot-Static Probes
SAE Technical Papers | 2022
Ice and Rain Minimum Qualification Standards for Pitot and Pitot-static Probes
SAE Technical Papers | 2020
Pitot or Pitot-Static Pressure Tubes, Electrically Heated (Turbine Powered Sub-Sonic Aircraft)
SAE Technical Papers | 2008
AIRSPEED INDICATOR (PITOT STATIC)
SAE Technical Papers | 1954
Springer Verlag | 2018
|