Studies Of The Leading Edge Effect On The Rarefied Hypersonic Flow Over A Flat Plate
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Author | : William Whyte Joss |
Publisher | : |
Total Pages | : 7 |
Release | : 1968 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Studies of the Leading Edge Effect on the Rarefied Hypersonic Flow Over a Flat Plate Book in PDF, Epub and Kindle
Author | : K. S. Heffner |
Publisher | : |
Total Pages | : |
Release | : 1991 |
Genre | : |
ISBN | : |
Download Leading Edge Effect on Rarefied Hypersonic Flow Over a Flat Plate Book in PDF, Epub and Kindle
Author | : William Whyte Joss |
Publisher | : |
Total Pages | : |
Release | : 1971 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download An Experimental Study of the Effects of Small Leading Edge Thickness on the Development of the Hypersonic Rarefied Flow Over a Flat Plate Book in PDF, Epub and Kindle
Author | : Andrew G. Hammitt |
Publisher | : |
Total Pages | : 16 |
Release | : 1956* |
Genre | : |
ISBN | : |
Download Hypersonic Studies of the Leading Edge Effect on the Flow Over a Flat Plate Book in PDF, Epub and Kindle
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 38 |
Release | : 2018-07-05 |
Genre | : |
ISBN | : 9781722316297 |
Download Interference Effects on the Hypersonic, Rarefied Flow about a Flat Plate Book in PDF, Epub and Kindle
The Direct Simulation Monte Carlo method is used to study the hypersonic, rarified flow interference effects on a flat plate caused by nearby surfaces. Calculations focus on shock-boundary-layer and shock-lip interactions in hypersonic inlets. Results are presented for geometries consisting of a flat plate with different leading-edge shapes over a flat lower wall and a blunt-edge flat plate over a 5-degree wedge. The problems simulated correspond to a typical entry flight condition of 7.5 km/s at altitudes of 75 to 90 km. The results show increases in predicted local heating rates for shock-boundary-layer and shock-lip interactions that are quantitatively similar to those observed experimentally at much higher densities. Wilmoth, Richard G. Langley Research Center RTOP 506-40-91-02...
Author | : R. E. Street |
Publisher | : |
Total Pages | : |
Release | : 1961 |
Genre | : |
ISBN | : |
Download Effect of Slip on the Laminar Boundary Layer Near the Leading Edge of a Flat Plate in Hypersonic Rarefied Gas Flow Book in PDF, Epub and Kindle
Author | : Goromir Goromirovich Chernyĭ |
Publisher | : |
Total Pages | : 24 |
Release | : 1960 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds Book in PDF, Epub and Kindle
Author | : Rateb Jaber El Assar |
Publisher | : |
Total Pages | : 106 |
Release | : 1968 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Kinetic Study of the Hypersonic Flow Past the Leading Edge of a Flat Plate Book in PDF, Epub and Kindle
Author | : W. J. McCroskey |
Publisher | : |
Total Pages | : 0 |
Release | : 1966 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download An Experimental Model for the Sharp Leading Edge Problem in Rarefied Hypersonic Flow Book in PDF, Epub and Kindle
Flow field studies of the shock wave and boundary layer development on a sharp flat plate are presented for a region of rarefied flow that bridges the gap between a classical hypersonic boundary layer downstream and a kinetic flow model at the leading edge. The measurements give a comprehensive picture of the flow pattern in the 'merged layer' or 'viscous layer' regime, which exists upstream of the region of validity of hypersonic viscous interaction theory. The results are derived from a combination of several probing and optical techniques and surface pressure measurements. From the detailed measurements, a true scale physical model of the flow field is constructed for the merged layer regime. One of the main features of the model is a thick, curved shock wave which decreases in strength as the leading edge is approached, even though the shock angle increases. Density profiles across the shock and viscous layers show that the structure of the flow field is quite different from the classical picture of a hypersonic boundary layer beneath an oblique Rankine-Hugonio shock wave. (Author).
Author | : R. J. El-Assar |
Publisher | : |
Total Pages | : 9 |
Release | : 1970 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download A Kinetic Study of the Hypersonic Flow Past the Leading Edge of a Flat Plate Book in PDF, Epub and Kindle