Experimental Wake Survey Behind A 140 Included Angle Cone At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
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Experimental Wake Survey Behind A 140 Included Angle Cone At Angles Of Attack Od 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
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Author : Clarence A. Jr Brown
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 140 Included Angle Cone At Angles Of Attack Od 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by Clarence A. Jr Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Experimental Wake Survey Behind A 140 Included Angle Cone At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
DOWNLOAD
Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 140 Included Angle Cone At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Angle of attack (Aerodynamics) categories.
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
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Author :
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Experimental Wake Survey Behind A 120 Included Angle Cone At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
DOWNLOAD
Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 120 Included Angle Cone At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Experimental Wake Survey Behind Viking 75 Entry Vehicle At Angles Of Attack Of 0 And 5 Mach Numbers From 20 To 1 20 And Longitudinal Stations From 1 50 To 11 00 Body Diameters
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Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1973
Experimental Wake Survey Behind Viking 75 Entry Vehicle At Angles Of Attack Of 0 And 5 Mach Numbers From 20 To 1 20 And Longitudinal Stations From 1 50 To 11 00 Body Diameters written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Flow visualization categories.
Experimental Wake Survey Behind Viking 1975 Entry Vehicle At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations From 1 0 To 8 39 Body Diameters
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Author :
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind Viking 1975 Entry Vehicle At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations From 1 0 To 8 39 Body Diameters written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Experimental Wake Survey Behind Viking 75 Entry Vehicle At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations From 1 0 To 8 39 Body Diameters
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Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind Viking 75 Entry Vehicle At Angles Of Attack Of 0 And 5 Mach Numbers From 1 60 To 3 95 And Longitudinal Stations From 1 0 To 8 39 Body Diameters written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
An investigation was conducted to obtain flow properties in the wake of the Viking '75 entry vehicle at mach numbers from 1.60 to 3.95 and at angles of attack of 0 deg and 5 deg. The wake flow properties were calculated from total and static pressures measured with a pressure rake at longitudinal stations varying from 1.0 to 8.39 body diameters and lateral stations varying from -0.42 to 3.0 body diameters. These measurements showed a consistent trend throughout the range of mach numbers and longitudinal distances and an increase in dynamic pressure with increasing downstream position.
Evaluation Of Flow Properties Behind 120 And 140 Included Angle Cones And A Viking 75 Entry Vehicle At Mach Numbers From 1 60 To 3 95
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Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1973
Evaluation Of Flow Properties Behind 120 And 140 Included Angle Cones And A Viking 75 Entry Vehicle At Mach Numbers From 1 60 To 3 95 written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Cone categories.
An Experimental Study Of The Turbulent Wake Behind A Cone At Mach 5
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Author : William C. Ragsdale
language : en
Publisher:
Release Date : 1966
An Experimental Study Of The Turbulent Wake Behind A Cone At Mach 5 written by William C. Ragsdale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Turbulence categories.
An experimental study of the turbulent wake behind a 9° adiabatic cone at Mach 5 has been carried out in the U.S. Naval Ordnance Laboratory Hypersonic Tunnel. Cone models with base diameters of 2 inches and 4 inches were mounted in the wind tunnel test section with fine wires. Pitot pressure, pressure on a small cone probe and total temperature were measured with probes mounted on a vertical traversing mechanism. The measured pressures and temperatures were used to calculate the Mach number, static pressure, static temperature, velocity and density in the wake.
Effects Of Reynolds Number And Model Support On The Supersonic Aerodynamic Chacteristics Of A 140 Included Angle Cone
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Author : Charles D. Trescot
language : en
Publisher:
Release Date : 1974
Effects Of Reynolds Number And Model Support On The Supersonic Aerodynamic Chacteristics Of A 140 Included Angle Cone written by Charles D. Trescot and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
An investigation has been made in the Langley Unitary Plan wind tunnel to determine the effects of Reynolds number and sting-support interference on the static aerodynamic characteristics of a 140 deg-included-angle cone. Base pressures and forces and moments of the model were measured at Mach numbers of 1.50, 2.00, 2.94, and 4.00 for ratios of sting diameter to model diameter that varied from 0.125 to 0.500 through an angle-of-attack range from about minus 4 deg to 13 deg. The Reynolds number, based on model diameter 4.80 in. was varied from 161,000 to 415,000.