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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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Book Synopsis Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 and 8 data for expansion corner flows by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 and 8 data for expansion corner flows written by Louis G. Kaufman and published by . This book was released on 1963 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: "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.
Book Synopsis Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 pressure data for flows ahead of ramps by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 pressure data for flows ahead of ramps written by Louis G. Kaufman and published by . This book was released on 1963 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt: "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.
Book Synopsis Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 pressure data for flows ahead of ramps by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 pressure data for flows ahead of ramps written by Louis G. Kaufman and published by . This book was released on 1964 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: "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.
Book Synopsis Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 heat transfer data for flows ahead of ramps by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 heat transfer data for flows ahead of ramps written by Louis G. Kaufman and published by . This book was released on 1964 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt: "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.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1964 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model by : Louis G. Kaufman (II.)
Download or read book Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model written by Louis G. Kaufman (II.) and published by . This book was released on 1964 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1967 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 474 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model by : Louis G. Kaufman
Download or read book Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model written by Louis G. Kaufman and published by . This book was released on 1964 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Pressure data for dihedral surfaces by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Pressure data for dihedral surfaces written by Louis G. Kaufman and published by . This book was released on 1964 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pryamidal Configuration with Aerodynamic Controls by : Louis G. Kaufman (II.)
Download or read book Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pryamidal Configuration with Aerodynamic Controls written by Louis G. Kaufman (II.) and published by . This book was released on 1964 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls by : Louis G. Kaufman
Download or read book Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls written by Louis G. Kaufman and published by . This book was released on 1964 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure data were obtained for Mach five flows over winged re-entry configurations composed of cylindrical cabins mounted on a 60 degree sweepback delta wing with a cylindrical leading edge, clipped tips, and trailing edge flaps. The model was tested with spherical and conical fronts on the cabin, with and without tip fins, and with and without a trailing edge spoiler. Flap deflections were varied from -40 to +40 degrees and the model was pitched at angles of attack from -30 to +45 degrees for a free stream Reynolds number, based on model length of 3,575,000. (Author)
Book Synopsis Heat-transfer Measurements at Mach 8 on a Flat Plate with Deflected Trailing-edge Flap with Effects of Transition Included by : Charles Borden Johnson
Download or read book Heat-transfer Measurements at Mach 8 on a Flat Plate with Deflected Trailing-edge Flap with Effects of Transition Included written by Charles Borden Johnson and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls by : Louis G. Kaufman
Download or read book Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls written by Louis G. Kaufman and published by . This book was released on 1964 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Heat transfer data for delta wing surface by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Heat transfer data for delta wing surface written by Louis G. Kaufman and published by . This book was released on 1964 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Flow-field Study at Mach Number 8 of Flow Separation on a Flat Plate with Deflected Trailing-edge Flap by : Charles B. Johnson
Download or read book Pressure and Flow-field Study at Mach Number 8 of Flow Separation on a Flat Plate with Deflected Trailing-edge Flap written by Charles B. Johnson and published by . This book was released on 1968 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
