Reynolds Number Effects At High Angles Of Attack
DOWNLOAD
AUDIOBOOK
READ ONLINE
Download Reynolds Number Effects At High Angles Of Attack PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Reynolds Number Effects At High Angles Of Attack book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
A Review Of Some Reynolds Number Effects Related To Bodies At High Angles Of Attack
DOWNLOAD
AUDIOBOOK
READ ONLINE
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.
Effects Of Reynolds Number And Body Corner Radius On Aerodynamic Characteristics Of A Space Shuttle Type Vehicle At Subsonic Mach Numbers
DOWNLOAD
AUDIOBOOK
READ ONLINE
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.
Effects Of Reynolds Number And Flow Incidence On The Force Characteristics Of A Family Of Flat Front Cylinders
DOWNLOAD
AUDIOBOOK
READ ONLINE
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.
Effect Of Flow Incidence And Reynolds Number On Low Speed Aerodynamic Characteristics Of Several Noncircular Cylinders With Applications To Directional Stability And Spinning
DOWNLOAD
AUDIOBOOK
READ ONLINE
Author : Edward Charles Polhamus
language : en
Publisher:
Release Date : 1959
Effect Of Flow Incidence And Reynolds Number On Low Speed Aerodynamic Characteristics Of Several Noncircular Cylinders With Applications To Directional Stability And Spinning written by Edward Charles Polhamus and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Cylinders categories.
Experimental Study Of The Effects Of Reynolds Number On High Angle Of Attack Aerodynamic Characteristics Of Forebodies During Rotary Motion
DOWNLOAD
AUDIOBOOK
READ ONLINE
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.
Reynolds Number Influences In Aeronautics
DOWNLOAD
AUDIOBOOK
READ ONLINE
Author :
language : en
Publisher:
Release Date : 1993
Reynolds Number Influences In Aeronautics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with categories.
Effect Of Unit Reynolds Number Nose Bluntness Angle Of Attack And Roughness On Transition On A 5 Half Angle Cone At Mach 8
DOWNLOAD
AUDIOBOOK
READ ONLINE
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.
Aerodynamics Of The Model Airplane Airfoil Measurements
DOWNLOAD
AUDIOBOOK
READ ONLINE
Author : Franz Wilhelm Schmitz
language : en
Publisher:
Release Date : 1967
Aerodynamics Of The Model Airplane Airfoil Measurements written by Franz Wilhelm Schmitz 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 categories.
A Reynolds Number Study Of Wing Leading Edge Effects On A Supersonic Transport Model At Mach 0 3
DOWNLOAD
AUDIOBOOK
READ ONLINE
Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-13
A Reynolds Number Study Of Wing Leading Edge Effects On A Supersonic Transport Model At Mach 0 3 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 2018-06-13 with categories.
A representative supersonic transport design was tested in the National Transonic Facility (NTF) in its original configuration with small-radius leading-edge flaps and also with modified large-radius inboard leading-edge flaps. Aerodynamic data were obtained over a range of Reynolds numbers at a Mach number of 0.3 and angles of attack up to 16 deg. Increasing the radius of the inboard leading-edge flap delayed nose-up pitching moment to a higher lift coefficient. Deflecting the large-radius leading-edge flap produced an overall decrease in lift coefficient and delayed nose-up pitching moment to even higher angles of attack as compared with the undeflected large- radius leading-edge flap. At angles of attack corresponding to the maximum untrimmed lift-to-drag ratio, lift and drag coefficients decreased while lift-to-drag ratio increased with increasing Reynolds number. At an angle of attack of 13.5 deg., the pitching-moment coefficient was nearly constant with increasing Reynolds number for both the small-radius leading-edge flap and the deflected large-radius leading-edge flap. However, the pitching moment coefficient increased with increasing Reynolds number for the undeflected large-radius leading-edge flap above a chord Reynolds number of about 35 x 10 (exp 6). Williams, M. Susan and Owens, Lewis R., Jr. and Chu, Julio Langley Research Center RTOP 537-03-22-06
Longitudinal Aerodynamic Characteristics Of Two Blunted Cone Reentry Configurations At Mach Numbers From 17 6 To 22 2 Including Some Reynolds Number Effects
DOWNLOAD
AUDIOBOOK
READ ONLINE
Author : Dal V. Maddalon
language : en
Publisher:
Release Date : 1966
Longitudinal Aerodynamic Characteristics Of Two Blunted Cone Reentry Configurations At Mach Numbers From 17 6 To 22 2 Including Some Reynolds Number Effects written by Dal V. Maddalon and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Cone categories.