Experimental Investigation of the Effect of Yaw on Rates of Heat Transfer to Transverse Circular Cylinders in a 6500-foot-per-second Hypersonic Air Stream
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Cunningham, Bernard E↗
Engineering topics
Kraus, Samuel
Publications and source records attributed to Kraus, Samuel.
Reductions in temperature-recovery factor associated with pulsating flows generated by spike-nosed cylinders at a Mach number of 3.50
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Hermach, C A↗
A study of inviscid flow about airfoils at high supersonic speeds
Steady flow about curved airfoils is investigated analytically, first assuming air behaves as an ideal gas, and then assuming it behaves as a thermally perfect, calorically imperfect gas. Conclusions are drawn from the study.
Eggers, A J↗
An Analysis of Supersonic Flow in the Region of the Leading Edge of Curved Airfoils, Including Charts for Determining Surface-pressure Gradient and Shock-wave Curvature
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Kraus, Samuel↗