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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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Download 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 PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get 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 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

Measurements Of Section Characteristics Of A 45 Degree Swept Wing Spanning A Rectangular Low Speed Wind Tunnel As Affected By The Tunnel Walls

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Author : Robert E. Dannenberg
language : en
Publisher:
Release Date : 1950

Measurements Of Section Characteristics Of A 45 Degree Swept Wing Spanning A Rectangular Low Speed Wind Tunnel As Affected By The Tunnel Walls written by Robert E. Dannenberg and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamic load categories.

Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.

Research Abstracts

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

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 1951 with Aeronautics categories.

Theory And Procedure For Determining Loads And Motions In Chine Immersed Hydrodynamic Impacts Of Prismatic Bodies

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Author : Emanuel Schnitzer
language : en
Publisher:
Release Date : 1952

Theory And Procedure For Determining Loads And Motions In Chine Immersed Hydrodynamic Impacts Of Prismatic Bodies written by Emanuel Schnitzer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Impact categories.

A theoretical method is derived for computing the motions and hydrodynamic loads during water landings of prismatic bodies involving appreciable immersion of the chines. A simplified method of computation covering flat-plate and V-bottom bodies with beam-loading coefficients greater than unity is given as a separate section. Comparisons of theory with experiment are presented as plots of impact lift coefficient and maximum draft-beam ratio against flight-path angle and as time histories of loads and motions. Fair agreement is found to exist for chine-immersed landings for angles of dead rise of 0 degrees and 30 degrees, beam-loading coefficients from 1 to 36.5, flight-path angles from 2 to 90 degrees, and trims from 6 to 45 degrees.

Technical Note National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957

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 1957 with Aeronautics categories.

Index Of Naca Technical Publications

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956

Index Of Naca Technical Publications 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 1956 with Aeronautics categories.