A Review Of Some Reynolds Number Effects Related To Bodies At High Angles Of Attack
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A Review Of Some Reynolds Number Effects Related To Bodies At High Angles Of Attack
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Author : Edward C. Polhamus
language : en
Publisher:
Release Date : 1984
A Review Of Some Reynolds Number Effects Related To Bodies At High Angles Of Attack written by Edward C. Polhamus and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Aerodynamics categories.
Experimental Study Of The Effects Of Reynolds Number On High Angle Of Attack Aerodynamic Characteristics Of Forebodies During Rotary Motion
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Author :
language : en
Publisher:
Release Date : 1995
Experimental Study Of The Effects Of Reynolds Number On High Angle Of Attack Aerodynamic Characteristics Of Forebodies During Rotary Motion written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with categories.
Effects Of Reynolds Number And Body Corner Radius On Aerodynamic Characteristics Of A Space Shuttle Type Vehicle At Subsonic Mach Numbers
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Author : Leland Howard Jorgenson
language : en
Publisher:
Release Date : 1972
Effects Of Reynolds Number And Body Corner Radius On Aerodynamic Characteristics Of A Space Shuttle Type Vehicle At Subsonic Mach Numbers written by Leland Howard Jorgenson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics categories.
Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Effect Of Unit Reynolds Number Nose Bluntness Angle Of Attack And Roughness On Transition On A 5 Half Angle Cone At Mach 8
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Author : P. Calvin Stainback
language : en
Publisher:
Release Date : 1969
Effect Of Unit Reynolds Number Nose Bluntness Angle Of Attack And Roughness On Transition On A 5 Half Angle Cone At Mach 8 written by P. Calvin Stainback and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamics, Hypersonic categories.
Navier Stokes Flight And Wind Tunnel Flow Analysis For The F A 18 Aircraft
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Author : Farhad Ghaffari
language : en
Publisher:
Release Date : 1994
Navier Stokes Flight And Wind Tunnel Flow Analysis For The F A 18 Aircraft written by Farhad Ghaffari and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Hornet (Jet fighter plane) categories.
Effects Of Reynolds Number And Flow Incidence On The Force Characteristics Of A Family Of Flat Front Cylinders
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Author : Vernard E. Lockwood
language : en
Publisher:
Release Date : 1967
Effects Of Reynolds Number And Flow Incidence On The Force Characteristics Of A Family Of Flat Front Cylinders written by Vernard E. Lockwood and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aerodynamics, Supersonic categories.
Scale Effects On Aircraft And Weapon Aerodynamics
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Author : A. B. Haines
language : en
Publisher:
Release Date : 1994
Scale Effects On Aircraft And Weapon Aerodynamics written by A. B. Haines and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aerodynamics categories.
Pressure Distributions On Three Bodies Of Revolution To Determine The Effect Of Reynolds Number Up To And Including The Transonic Speed Range
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Author : John M. Swihart
language : en
Publisher:
Release Date : 1953
Pressure Distributions On Three Bodies Of Revolution To Determine The Effect Of Reynolds Number Up To And Including The Transonic Speed Range written by John M. Swihart and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aerodynamics, Transonic categories.
Abstract: The effects of varying Reynolds number on the pressure distribution over a transonic body of revolution are presented. Angles of attack from -2° to 15° were investigated through a Mach number range from 0.60 to 1.09. The Reynolds number based on body length varied from 9 x 106 to 39 x 106, and on maximum diameter from 1.35 x 105 to 4.53 x 105. There were small effects of Reynolds number on the axial pressure distributions of these bodies. These effects were of such a nature as to cause an increase of 0.05 in the normal-force coefficient of the body when tested in the subcritical cross-flow Reynolds number range. A comparison between values of incremental pressure coefficient due to angle of attack and theoretical values was made.
Simulation Of Forebody Flows At High Angle Of Attack Rotary Conditions
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Author : Syta Saephan
language : en
Publisher:
Release Date : 2002
Simulation Of Forebody Flows At High Angle Of Attack Rotary Conditions written by Syta Saephan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with categories.