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Results Of Aerothermodynamic And Boundary Layer Transition Testing Of 00362 Scale X 38 Rev 31 Vehicle In Nasa Langley 20 Inch Mach 6 Tunnel
Download Results Of Aerothermodynamic And Boundary Layer Transition Testing Of 00362 Scale X 38 Rev 31 Vehicle In Nasa Langley 20 Inch Mach 6 Tunnel full books in PDF, epub, and Kindle. Read online Results Of Aerothermodynamic And Boundary Layer Transition Testing Of 00362 Scale X 38 Rev 31 Vehicle In Nasa Langley 20 Inch Mach 6 Tunnel ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis 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 by :
Download or read book 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 written by and published by . This book was released on 1997 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Results Of Aerothermodynamic And Boundary-Layer Transition Testing Of 0.0362-Scale X-38 (Rev. 3.1) Vehicles In NASA... NASA-TM-112857... Oct. 31, 1997 by : United States. National Aeronautics and Space Administration
Download or read book Results Of Aerothermodynamic And Boundary-Layer Transition Testing Of 0.0362-Scale X-38 (Rev. 3.1) Vehicles In NASA... NASA-TM-112857... Oct. 31, 1997 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1998* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel by :
Download or read book Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel written by and published by . This book was released on 2000 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720558514 Total Pages :64 pages Book Rating :4.5/5 (585 download)
Book Synopsis Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-31 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aeroheating and boundary layer transition characteristics for the X-43 (Hyper-X) configuration have been experimentally examined in the Langley 20-Inch Mach 6 Air Tunnel. Global surface heat transfer distributions, and surface streamline patterns were measured on a 0.333-scale model of the Hyper-X forebody. Parametric variations include angles-of-attack of 0-deg, 2-deg, and 4-deg; Reynolds numbers based on model length of 1.2 to 15.4 million; and inlet cowl door both open and closed. The effects of discrete roughness elements on the forebody boundary layer, which included variations in trip configuration and height, were investigated. This document is intended to serve as a release of preliminary data to the Hyper-X program; analysis is limited to observations of the experimental trends in order to expedite dissemination.Berry, Scott A. and DiFulvio, Michael and Kowalkowski, Matthew K.Langley Research CenterAERODYNAMIC HEATING; BOUNDARY LAYER TRANSITION; WIND TUNNEL TESTS; SCALE MODELS; HEAT TRANSFER; HYPERSONIC FLIGHT; THERMOGRAPHY; ANGLE OF ATTACK; REYNOLDS NUMBER; HYPERSONIC SPEED; X-43 VEHICLE
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720558590 Total Pages :78 pages Book Rating :4.5/5 (585 download)
Book Synopsis Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 31 Mach 10 Air Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 31 Mach 10 Air Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-31 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aeroheating and boundary layer transition characteristics for the X-43 (Hyper-X) configuration have been experimentally examined in the Langley 31-Inch Mach 10 Air Tunnel. Global surface heat transfer distributions, and surface streamline patterns were measured on a 0.333-scale model of the Hyper-X forebody. Parametric variations include angles-of-attack of 0-deg, 2-deg, 3-deg, and 4-deg; Reynolds numbers based on model length of 1.2 to 5.1 million; and inlet cowl door both open and closed. The effects of discrete roughness elements on the forebody boundary layer, which included variations in trip configuration and height, were investigated. This document is intended to serve as a release of preliminary data to the Hyper-X program; analysis is limited to observations of the experimental trends in order to expedite dissemination.Administration (NASA)Langley Research CenterAERODYNAMIC HEATING; BOUNDARY LAYER TRANSITION; WIND TUNNEL TESTS; SCALE MODELS; HEAT TRANSFER; THERMOGRAPHY; HYPERSONIC FLIGHT; X-43 VEHICLE; REYNOLDS NUMBER; ANGLE OF ATTACK; HYPERSONIC SPEED
Book Synopsis Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 31-Inch Mach 10 Air Tunnel by :
Download or read book Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 31-Inch Mach 10 Air Tunnel written by and published by . This book was released on 2000 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
