[PDF] An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw - eBooks Review

An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw


An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw
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An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw


An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw
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Author : Franklin K. Moore
language : en
Publisher:
Release Date : 1956

An Analysis Of Once Per Revolution Oscillating Aerodynamic Thrust Loads On Single Rotation Propellers On Tractor Airplanes At Zero Yaw written by Franklin K. Moore 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.




Report


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

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 1956 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 : 1957

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 1957 with Aeronautics categories.


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



Report


Report
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Author :
language : en
Publisher:
Release Date : 1956

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 1956 with Aeronautics categories.




Monthly Catalog Of United States Government Publications


Monthly Catalog Of United States Government Publications
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1957

Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Government publications categories.


February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.



Annual Report


Annual Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1953

Annual 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 1953 with Aeronautics categories.




A Wind Tunnel Investigation Of Three Propellers Through An Angle Of Attack Range From 0 Degree To 85 Degrees


A Wind Tunnel Investigation Of Three Propellers Through An Angle Of Attack Range From 0 Degree To 85 Degrees
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Author : Paul F. Yaggy
language : en
Publisher:
Release Date : 1960

A Wind Tunnel Investigation Of Three Propellers Through An Angle Of Attack Range From 0 Degree To 85 Degrees written by Paul F. Yaggy and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Propellers, Aerial categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1960

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 1960 with 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.




Axially Symmetric Shapes With Minimum Wave Drag


Axially Symmetric Shapes With Minimum Wave Drag
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Author : Maxwell Alfred Heaslet
language : en
Publisher:
Release Date : 1955

Axially Symmetric Shapes With Minimum Wave Drag written by Maxwell Alfred Heaslet 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.


The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either in terms of the geometry of the body, or in terms of the body-simulating axial source distribution. For purposes of deriving optimum bodies under various given condtions, it is found that the second of the methods mentioned is the more tractable. By use of a quasi-cylindrical theory, that is, the boundary conditions are applied on the surface of a cylinder rather than on the body itself, the variational problems of the optimum bodies having prescribed volume or caliber are solved. The streamwise variations of cross-section area and drags of the bodies are exhibited, and some numerical results are given. The solutions are found to depend upon a single parameter involving Mach number and radius-lenght ration of the given cylinder. Variation of this parameter from zero to infinity gives the spectrum of optimum bodies with the given condition from the slender-body result of the two-dimensional. The numerical results show that for increasing values of the parameter, the optimum shapes quickly approach the two-dimensional.