[PDF] Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5 - eBooks Review

Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5


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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Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5


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.



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


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.




Experimental Determination Of Effects Of Frequency And Amplitude On The Lateral Stability Derivatives For A Delta A Swept And An Upswept Wing Oscillating In Yaw


Experimental Determination Of Effects Of Frequency And Amplitude On The Lateral Stability Derivatives For A Delta A Swept And An Upswept Wing Oscillating In Yaw
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Author : Dean R. Chapman
language : en
Publisher:
Release Date : 1958

Experimental Determination Of Effects Of Frequency And Amplitude On The Lateral Stability Derivatives For A Delta A Swept And An Upswept Wing Oscillating In Yaw 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 1958 with Aerofoils categories.




Report


Report
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Author :
language : en
Publisher:
Release Date : 1957

Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.




Experimental Investigation Of The Effect Of Vertical Tail Size And Length And Of Fuselage Shape And Length On The Static Lateral Stability Characteristics Of A Model With 45 Sweptback Wing And Tail Surfaces


Experimental Investigation Of The Effect Of Vertical Tail Size And Length And Of Fuselage Shape And Length On The Static Lateral Stability Characteristics Of A Model With 45 Sweptback Wing And Tail Surfaces
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Author : Antonio Ferri
language : en
Publisher:
Release Date : 1951

Experimental Investigation Of The Effect Of Vertical Tail Size And Length And Of Fuselage Shape And Length On The Static Lateral Stability Characteristics Of A Model With 45 Sweptback Wing And Tail Surfaces written by Antonio Ferri 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.




Technical Note


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.




Report National Advisory Committee For Aeronautics


Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951

Report 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 1951 with Aeronautics categories.




Report


Report
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1958

Report 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 1958 with Aeronautics categories.




Technical Note National Advisory Committee For Aeronautics


Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1955

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 1955 with Aeronautics categories.




Annual Report National Advisory Committee For Aeronautics


Annual Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1955

Annual Report 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 1955 with Aeronautics categories.


Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.