Related Books

X-33 Rev-F Turbulent Aeroheating Results From Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons With Computations
Language: en
Pages: 76

X-33 Rev-F Turbulent Aeroheating Results From Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons With Computations

Authors: Brian R. Hollis
Categories: Aerothermodynamics
Type: BOOK - Published: 2003 - Publisher:

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X-33 Rev-F Turbulent Aeroheating Results from Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons with Computations
Language: en
Pages: 72

X-33 Rev-F Turbulent Aeroheating Results from Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons with Computations

Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-06-12 - Publisher: Createspace Independent Publishing Platform

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Measurements and predictions of the X-33 turbulent aeroheating environment have been performed at Mach 6, perfect-gas air conditions. The purpose of this invest
X-33 (Rev-F) Aeroheating Results of Test 6770 in NASA Langley 20-Inch Mach 6 Air Tunnel
Language: en
Pages: 100

X-33 (Rev-F) Aeroheating Results of Test 6770 in NASA Langley 20-Inch Mach 6 Air Tunnel

Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-06-12 - Publisher: Createspace Independent Publishing Platform

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Aeroheating characteristics of the X-33 Rev-F configuration have been experimentally examined in the Langley 20-Inch Mach 6 Air Tunnel (Test 6770). Global surfa
Scientific and Technical Aerospace Reports
Language: en
Pages: 456

Scientific and Technical Aerospace Reports

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1995 - Publisher:

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N
Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0. 0362-Scale X-38 (Rev. 3. 1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel
Language: en
Pages: 100

Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0. 0362-Scale X-38 (Rev. 3. 1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel

Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-13 - Publisher: Createspace Independent Publishing Platform

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The aeroheating characteristics of the X-38 Revision 3.1 lifting-body configuration have been experimentally examined in the Langley 20-inch Mach 6 Tunnel. Glob