Turbulent Boundary Layer Heat Transfer And Transition Measurements With Surface Cooling At Mach 6
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Author | : Aubrey M. Cary |
Publisher | : |
Total Pages | : 58 |
Release | : 1970 |
Genre | : Heat |
ISBN | : |
Download Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 Book in PDF, Epub and Kindle
Author | : Aubrey Cary |
Publisher | : |
Total Pages | : 154 |
Release | : 1969 |
Genre | : Boundary layer |
ISBN | : |
Download Turbulent Boundary Layer Heat Transfer and Transition Measurements with Extreme Surface Cooling in Hypersonic Flow Book in PDF, Epub and Kindle
Author | : Michael E. Tauber |
Publisher | : |
Total Pages | : 44 |
Release | : 1989 |
Genre | : Aerodynamic heating |
ISBN | : |
Download A Review of High-speed, Convective, Heat-transfer Computation Methods Book in PDF, Epub and Kindle
Author | : Victor Zakkay |
Publisher | : |
Total Pages | : 86 |
Release | : 1962 |
Genre | : Boundary layer |
ISBN | : |
Download Laminar, Transitional, and Turbulent Heat Transfer to a Cone-cylinder-flare Body at Mach 8.0 Book in PDF, Epub and Kindle
A modified equation for the heat transfer coefficient in the transitional and fully turbulent region based on the F.P.R.E. method is then presented. This method gives good agreement with the experimental results presented here.
Author | : Robert L. P. Voisinet |
Publisher | : |
Total Pages | : 128 |
Release | : 1972 |
Genre | : Heat |
ISBN | : |
Download Measurements of a Mach 4.9 Zero-pressure-gradient Turbulent Boundary Layer with Heat Yransfer Book in PDF, Epub and Kindle
The results of a detailed experimental investigation of the compressible turbulent boundary layer in a zero-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall for a nominal Mach number of 4.9, at momentum thickness Reynolds numbers from 7,000. to 58,000. and at wall-to-adiabatic-wall temperature ratios of 1.0, 0.8 and 0.25. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. Furthermore, the wall shear and surface heat transfer were measured directly with a skin-friction balance and a heat-transfer gage, respectively. (Author Modified Abstract).
Author | : Paul F. Brinich |
Publisher | : |
Total Pages | : 56 |
Release | : 1961 |
Genre | : |
ISBN | : |
Download Recovery Temperature Transition and Heat-transfer Measurements at Mach 5 Book in PDF, Epub and Kindle
Author | : Paige B. Burbank |
Publisher | : |
Total Pages | : 430 |
Release | : 1962 |
Genre | : Heat |
ISBN | : |
Download Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 596 |
Release | : 1973 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : L. H. Back |
Publisher | : |
Total Pages | : 11 |
Release | : 1969 |
Genre | : Heat |
ISBN | : |
Download Laminar, Transition, and Turbulent Boundary-layer Heat-transfer Measurements with Wall Cooling in Turbulent Airflow Through a Tube Book in PDF, Epub and Kindle
Author | : Raul Jorge Conti |
Publisher | : |
Total Pages | : 32 |
Release | : 1959 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution Book in PDF, Epub and Kindle