Pressure And Heat Transfer Measurements For Hypersonic Flows Over Expansion Corners And Ahead Of Ramps Mach 5 And 8 Data For Expansion Corner Flows
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| Author | : Louis G. Kaufman |
| Publisher | : |
| Total Pages | : 96 |
| Release | : 1963 |
| Genre | : Aerodynamic heating |
| ISBN | : |
"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.
| Author | : Louis G. Kaufman |
| Publisher | : |
| Total Pages | : 172 |
| Release | : 1964 |
| Genre | : Aerodynamic heating |
| ISBN | : |
"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.
| Author | : Louis G. Kaufman |
| Publisher | : |
| Total Pages | : 238 |
| Release | : 1963 |
| Genre | : Aerodynamic heating |
| ISBN | : |
"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.
| Author | : Louis G. Kaufman |
| Publisher | : |
| Total Pages | : 144 |
| Release | : 1964 |
| Genre | : Aerodynamic heating |
| ISBN | : |
"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.
| Author | : |
| Publisher | : |
| Total Pages | : 666 |
| Release | : 1964 |
| Genre | : Mechanics, Applied |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1416 |
| Release | : 1964 |
| Genre | : Science |
| ISBN | : |
| Author | : Louis G. Kaufman (II.) |
| Publisher | : |
| Total Pages | : 188 |
| Release | : 1964 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1388 |
| Release | : 1967 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 474 |
| Release | : 1970 |
| Genre | : |
| ISBN | : |
| Author | : Louis G. Kaufman |
| Publisher | : |
| Total Pages | : 164 |
| Release | : 1964 |
| Genre | : Aerodynamic load |
| ISBN | : |
The report presents data obtained on the upper, flat plate, surface of the model and on the face of a 25% chord, full span, ramp mounted on the trailing edge of the flat plate. Data were obtained for three ramp angles, both with and without internal cooling of the flat plate surface, for model angles of attack from -43 to +10 degrees for free stream Reynolds numbers per foot of 1.1, 2.2 and 3.3 million.
