Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers

@inproceedings{BECKWITHLocalHT,
  title={Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers},
  author={IVAN E. BECKWITH}
}
  • IVAN E. BECKWITH

References

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Showing 1-4 of 4 references

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

Cunningham, E Bernard, Kraus, Samuel
NACA RM A58E19, • 1958

Free-Flight Investigation of Aerodynamic Heat' Transfer to a Simulated GlideRocket Shape at Mach Numbers up to 10

Swanson, G Andrew
NACA RM L58G03, • 1958

Investigation of Local Heat-Transfer and Pressure Drag Characteristics of a Yawed Circular Cylinder at Supersonic Speeds

Goodwin, Glen, +3 authors L Ernest
NACA RM A55H31, • 1956

Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9

Feller, V William
NACA RM L55F08a, • 1955

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