Wind Tunnel Tests Of A Two Thirds Scale Nasa Hre Inlet At Mach Numbers 4 5 6 And 8
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Author | : Frederick K. Hube |
Publisher | : |
Total Pages | : 60 |
Release | : 1969 |
Genre | : |
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Download Wind Tunnel Tests of a Two-Thirds Scale NASA HRE Inlet at Mach Numbers 4, 5, 6, and 8 Book in PDF, Epub and Kindle
An axisymmetric, variable geometry, two-thirds scale model of a NASA Hypersonic Research Engine (HRE) inlet was tested at Mach numbers 4, 5, 6, and 8. Surface pressures and temperatures were measured on the inlet centerbody and inside the cowl. Pitot pressure measurements were made at four stations along the internal passage. The measurements were obtained for various cowl positions at free-stream Reynolds numbers from 1.08 to 5.76 million (based on a 12-in. cowl diameter) and over an angle-of-attack range from -5 to +5 deg. The model walls were internally cooled and maintained at a minimum frost-free condition at each test condition. Selected results are presented to illustrate the effects of cowl position, angle of attack, Mach number, and Reynolds number on the surface and rake station measurements. Inlet performance data at design operating conditions are also presented. (Author).
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1969 |
Genre | : |
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Download Wind Tunnel Tests of a Two-Thirds Scale NASA HRE Inlet at Mach Numbers 4, 5, 6, and 8 Book in PDF, Epub and Kindle
An axisymmetric, variable geometry, two-thirds scale model of a NASA Hypersonic Research Engine (HRE) inlet was tested at Mach numbers 4, 5, 6, and 8. Surface pressures and temperatures were measured on the inlet centerbody and inside the cowl. Pitot pressure measurements were made at four stations along the internal passage. The measurements were obtained for various cowl positions at free-stream Reynolds numbers from 1.08 to 5.76 million (based on a 12-in. cowl diameter) and over an angle-of-attack range from -5 to +5 deg. The model walls were internally cooled and maintained at a minimum frost-free condition at each test condition. Selected results are presented to illustrate the effects of cowl position, angle of attack, Mach number, and Reynolds number on the surface and rake station measurements. Inlet performance data at design operating conditions are also presented. (Author).
Author | : |
Publisher | : |
Total Pages | : 702 |
Release | : 1976 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Memorandum Book in PDF, Epub and Kindle
Author | : Earl H. Andrews |
Publisher | : |
Total Pages | : 56 |
Release | : 1976 |
Genre | : Jet engines |
ISBN | : |
Download Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model Book in PDF, Epub and Kindle
Author | : Earl H. Andrews |
Publisher | : |
Total Pages | : 60 |
Release | : 1994 |
Genre | : Airplanes |
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Download NASA's Hypersonic Research Engine Project Book in PDF, Epub and Kindle
Author | : |
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Total Pages | : 58 |
Release | : 1994 |
Genre | : |
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Download NASA's Hypersonic Research Engine Project: A Review Book in PDF, Epub and Kindle
Author | : Warren H. Philipp |
Publisher | : |
Total Pages | : 678 |
Release | : 1976 |
Genre | : Electric batteries |
ISBN | : |
Download Functioning of Inorganic/organic Battery Separators in Silver-zinc Cells Book in PDF, Epub and Kindle
Author | : Frederick K. Hube |
Publisher | : |
Total Pages | : 278 |
Release | : 1970 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0 Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 52 |
Release | : 1974 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download An Inlet Analysis for the NASA Hypersonic Research Engine Aerothermodynamic Integration Model Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 636 |
Release | : 1992 |
Genre | : Airplanes |
ISBN | : |
Download 93-2300 - 93-2349 Book in PDF, Epub and Kindle