Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Nasa Tm 4645 Vol 2 Mar
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Journal Of Aircraft
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Author :
language : en
Publisher:
Release Date : 2009
Journal Of Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2009 with Aeronautics categories.
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Nasa Tm 4645 Vol 2 Mar
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Author :
language : en
Publisher:
Release Date : 1998
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Nasa Tm 4645 Vol 2 Mar written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1996-09
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996-09 with Science categories.
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Volume 2 Small Radius Leading Edge
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-24
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Volume 2 Small Radius Leading Edge written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-24 with categories.
An experimental wind tunnel test of a 65 deg. delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF). The objective was to investigate the effects of Reynolds and Mach numbers on slender-wing leading-edge vortex flows with four values of wing leading-edge bluntness. Experimentally obtained pressure data are presented without analysis in tabulated and graphical formats across a Reynolds number range of 6 x 10(exp 6) to 84 x 10(exp 6) at a Mach number of 0.85 and across a Mach number range of 0.4 to 0.9 at Reynolds numbers of 6 x 10(exp 6) and 60 x 10(exp 6). Normal-force and pitching-moment coefficient plots for these Reynolds number and Mach number ranges are also presented. Chu, Julio and Luckring, James M. Langley Research Center NASA-TM-4645-Vol-2, L-17411B-Vol-2, NAS 1.15:4645-Vol-2 RTOP 505-59-54-01...
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Vol 4
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-24
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Vol 4 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-24 with categories.
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF). The objective was to investigate the effects of Reynolds and Mach numbers on slender-wing leading-edge vortex flows with four values of wing leading-edge bluntness. Experimentally obtained pressure data are presented without analysis in tabulated and graphical formats across a Reynolds number range of 6 x 10(exp 6) to 120 x 10(exp 6) at a Mach number of 0.85 and across a Mach number range of 0.4 to 0.9 at Reynolds numbers of 6 x 10(exp 6) and 60 x 10(exp 6). Normal-force and pitching-moment coefficient plots for these Reynolds number and Mach number ranges are also presented. Chu, Julio and Luckring, James M. Langley Research Center NASA-TM-4645-Vol-4, L-17411D-Vol-4, NAS 1.15:4645-Vol-4 RTOP 505-59-54-01...
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Volume 1 Sharp Leading Edge Conducted In The Langley National Transonic Facility Ntf
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-24
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Number And Mach Number Ranges Volume 1 Sharp Leading Edge Conducted In The Langley National Transonic Facility Ntf written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-24 with categories.
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF). The objective was to investigate the effects of Reynolds and Mach numbers on slender-wing leading-edge vortex flows with four values of wing leading-edge bluntness. Experimentally obtained pressure data are presented without analysis in tabulated and graphical formats across a Reynolds number range of 6 x 10(exp 6) to 36 x 10(exp 6) at a Mach number of 0.85 and across a Mach number range of 0.4 to 0.9 at a Reynolds number of 6 x 10(exp 6). Normal-force and pitching-moment coefficient plots for these Reynolds number and Mach number ranges are also presented. Chu, Julio and Luckring, James M. Langley Research Center NASA-TM-4645-Vol-1, L-17411A, NAS 1.15:4645-Vol-1 RTOP 505-59-54-01...
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges
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Author : Julio Chu
language : en
Publisher:
Release Date : 1996
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges written by Julio Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Angle of attack categories.
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges
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Author : Julio Chu
language : en
Publisher:
Release Date : 1996
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges written by Julio Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Angle of attack categories.
Experimental Surface Pressure Data Obtained On A 65 Degrees Delta Wing Across Reynolds Number And Mach Number Ranges
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Author : Julio Chu
language : en
Publisher:
Release Date : 1996
Experimental Surface Pressure Data Obtained On A 65 Degrees Delta Wing Across Reynolds Number And Mach Number Ranges written by Julio Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Nasa Tm 4645 Mar 14 1997
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1998*
Experimental Surface Pressure Data Obtained On 65 Deg Delta Wing Across Reynolds Nasa Tm 4645 Mar 14 1997 written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998* with categories.