On The Stability Of A Laminar Compressible Boundary Layer Over A Flat Plate Subject To Uniform Suction And Injection
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Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1957
Effects of Thermal Relaxation and Specific-heat Changes on Measurements with a Pneumatic-probe Pyrometer
Equations are derived to evaluate the effects of thermal vibration relaxation and specific-heat changes on pneumatic-probe pyrometer measurements in the region 1000 to 3000 degrees K and 0.3