Experimental Laminar Transitional And Turbulent Boundary Layer Profiles On A Wedge At Local Mach Number 65 And Comparisons With Theory PDF Download
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Author | : Michael C. Fischer |
Publisher | : |
Total Pages | : 66 |
Release | : 1971 |
Genre | : Boundary layer |
ISBN | : |
Download Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory Book in PDF, ePub and Kindle
Wind tunnel investigation of laminar, transitional, and turbulent boundary layer profiles on wedge at hypersonic speed to confirm theoretical analysis.
Author | : Michael C. Fischer |
Publisher | : |
Total Pages | : 58 |
Release | : 1971 |
Genre | : |
ISBN | : |
Download Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 814 |
Release | : 1978 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Paper Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 332 |
Release | : 1978 |
Genre | : Science |
ISBN | : |
Download NASA Technical Paper Book in PDF, ePub and Kindle
Author | : S. J. Shamroth |
Publisher | : |
Total Pages | : 76 |
Release | : 1972 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Assessment of a Transitional Boundary Layer Theory at Low Hypersonic Mach Numbers Book in PDF, ePub and Kindle
An investigation was carried out to assess the accuracy of a transitional boundary layer theory in the low hypersonic Mach number regime. The theory is based upon the simultaneous numerical solution of the boundary layer partial differential equations for the mean motion and an integral form of the turbulence kinetic energy equation which controls the magnitude and development of the Reynolds stress. Comparisions with experimental data show the theory is capable of accurately predicting heat transfer and velocity profiles through the transitional regime and correctly predicts the effects of Mach number and wall cooling on transition Reynolds number. The procedure shows promise of predicting the initiation of transition for given free stream disturbance levels. The effects on transition predictions of the pressure dilitation term and of direct absorption of acoustic energy by the boundary layer were evaluated.
Author | : Ralph D. Watson |
Publisher | : |
Total Pages | : 346 |
Release | : 1978 |
Genre | : Boundary layer |
ISBN | : |
Download Characteristics of Mach 10 Transitional and Turbulent Boundary Layers Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 814 |
Release | : 1973 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Contractor Report Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 282 |
Release | : 1971 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : S. J. Shamroth |
Publisher | : |
Total Pages | : 76 |
Release | : 1972 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Assessment of a Transitional Boundary Layer Theory at Low Hypersonic Mach Numbers Book in PDF, ePub and Kindle
An investigation was carried out to assess the accuracy of a transitional boundary layer theory in the low hypersonic Mach number regime. The theory is based upon the simultaneous numerical solution of the boundary layer partial differential equations for the mean motion and an integral form of the turbulence kinetic energy equation which controls the magnitude and development of the Reynolds stress. Comparisions with experimental data show the theory is capable of accurately predicting heat transfer and velocity profiles through the transitional regime and correctly predicts the effects of Mach number and wall cooling on transition Reynolds number. The procedure shows promise of predicting the initiation of transition for given free stream disturbance levels. The effects on transition predictions of the pressure dilitation term and of direct absorption of acoustic energy by the boundary layer were evaluated.
Author | : |
Publisher | : |
Total Pages | : 1388 |
Release | : 1971 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle