Experimental Investigation Of The Effects Of Support Interference On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5
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Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5
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Author : Dean R. Chapman
language : en
Publisher:
Release Date : 1947
Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5 written by Dean R. Chapman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aerodynamics categories.
Summary: Tests were conducted to determine the effects of viscosity on the drag and base pressure characteristics of various bodies of revolution at a Mach number of 1.5. The models were tested both with smooth surfaces and with roughness added to evaluate the effects of Reynolds number for both laminar and turbulent boundary layers. The principal geometric variables investigated were after-body shape and length-diameter ratio. For most models, force tests and base pressure measurements were made over a range of Reynolds numbers, based on model length, from 0.6 million to 5.0 millions. Schlieren photographs were used to analyze the effects of viscosity on flow separation and shock-wave configuration near the base and to verify the condition of the boundary layer as deduced from force tests. The results are discussed and compared with theoretical calculations.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1991
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1970
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.
An Experimental Investigation Of Sting Support Effects On Drag And A Comparison With Jet Effects At Transonic Speeds
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Author : Charles L. Shuford
language : en
Publisher:
Release Date : 1958
An Experimental Investigation Of Sting Support Effects On Drag And A Comparison With Jet Effects At Transonic Speeds written by Charles L. Shuford and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.
A Study Of The Use Of Experimental Stability Derivatives In The Calculation Of The Lateral Disturbed Motions Of A Swept Wing Airplane And Comparison With Flight Results
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Author : Carl Kaplan
language : en
Publisher:
Release Date : 1951
A Study Of The Use Of Experimental Stability Derivatives In The Calculation Of The Lateral Disturbed Motions Of A Swept Wing Airplane And Comparison With Flight Results written by Carl Kaplan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aerodynamics, Supersonic categories.
Research Abstracts
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
Research Abstracts written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.
The Effect Of Base Bleed On The Drag And Magnus Characteristics Of A Rotating Body Of Revolution
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Author : Frank J. Regan
language : en
Publisher:
Release Date : 1972
The Effect Of Base Bleed On The Drag And Magnus Characteristics Of A Rotating Body Of Revolution written by Frank J. Regan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Body of revolution categories.
Base bleed is a technique whereby all or part of the boundary layer is 'bled' from the rear portion of a projectile to the base region. Passage from the model's surface to the base region is by means of concentric cylindrical passageways. The purpose of base bleed is to reduce the Magnus moment on overlong spinning bodies of revolution and to reduce the base drag. Both analytic and experimental results are presented. The boundary layer is represented by means of the momentum thickness.
Naca Research Memorandum
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Author :
language : en
Publisher:
Release Date : 1950
Naca Research Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamics categories.
Technical Note
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Author :
language : en
Publisher:
Release Date : 1955
Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.