The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow


The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow


The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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Author : Arthur Leslie Jones
language : en
Publisher:
Release Date : 1949

The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur Leslie Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.


The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.



The Rolling Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow


The Rolling Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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Author : Arthur L. Jones
language : en
Publisher:
Release Date : 1948

The Rolling Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur L. Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aerodynamics, Supersonic categories.


The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.



Rolling And Yawing Moments For Swept Back Wings In Sideslip At Supersonic Sppeds


Rolling And Yawing Moments For Swept Back Wings In Sideslip At Supersonic Sppeds
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Author : Seymour Lampert
language : en
Publisher:
Release Date : 1951

Rolling And Yawing Moments For Swept Back Wings In Sideslip At Supersonic Sppeds written by Seymour Lampert 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.


A method is presented for determining the rolling and yawing moments of swept-back wings in steady sideslip at supersonic speeds. The case treated in particular is that of a swept tapered wing with all edges subsonic.



Use Of A Characteristic Surfaces For Unisymmetrical Supersonic Flow Problems


Use Of A Characteristic Surfaces For Unisymmetrical Supersonic Flow Problems
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Author : W. E. Moeckel
language : en
Publisher:
Release Date : 1949

Use Of A Characteristic Surfaces For Unisymmetrical Supersonic Flow Problems written by W. E. Moeckel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.


Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.



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 : 1953

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 1953 with Aeronautics categories.




Annual Report Of The National Advisory Committee For Aeronautics


Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954

Annual Report Of The 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.


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



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 : 1948

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 1948 with Aeronautics categories.




Report


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

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 1951 with Aeronautics categories.




Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations


Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations
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Author : Robert O. Piland
language : en
Publisher:
Release Date : 1951

Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations written by Robert O. Piland 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.


The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force and yawing moment due to rolling of a trapezoidal wing are derived. The equations are applicable when the inboard Mach line from a leading-edge tip intersects the trailing edge and the outboard Mach line lies ahead of the side edge. When the side edges are raked in, the former condition is sufficient. A comparison based on theoretical expressions of the lift and rolling effectiveness for half-delta tip (point forward) and trailing-edge flaps on various plan forms is made.



Aero Digest


Aero Digest
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Author :
language : en
Publisher:
Release Date : 1950

Aero Digest 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 Aeronautics categories.