Theoretical Investigation At Subsonic Speeds Of The Flow Ahead Of A Slender Inclined Parabolic Arc Body Of Revolution And Correlation With Experimental Data Obtained At Low Speeds

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Theoretical Investigation At Subsonic Speeds Of The Flow Ahead Of A Slender Inclinded Parabolic Arc Body Of Revolution And Correlation With Experimental Data Obtained At Low Speeds

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Author : William Letko
language : en
Publisher:
Release Date : 1954

Theoretical Investigation At Subsonic Speeds Of The Flow Ahead Of A Slender Inclinded Parabolic Arc Body Of Revolution And Correlation With Experimental Data Obtained At Low Speeds written by William Letko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics categories.

Subsonic linearized theory is used to derive approximate expressions for the incremental pressure coefficient and flow inclination ahead of slender profile-arc bodies of revolution alined (sic) with the stream and at samll angles of attack or sideslip.

Theoretical Investigation At Subsonic Speeds Of The Flow Ahead Of A Slender Inclined Parabolic Arc Body Of Revolution And Correlation With Experimental Data Obtained At Low Speeds

DOWNLOAD
Author : William Letko
language : en
Publisher:
Release Date : 1954

Theoretical Investigation At Subsonic Speeds Of The Flow Ahead Of A Slender Inclined Parabolic Arc Body Of Revolution And Correlation With Experimental Data Obtained At Low Speeds written by William Letko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with 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 : 1958

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 1958 with Aeronautics categories.

Technical Note

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Author :
language : en
Publisher:
Release Date : 1954

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 1954 with Aeronautics categories.

Hovering Flight Tests Of A Four Engine Transport Vertical Take Off Airplane Model Utilizing A Large Flap And Extensible Vanes For Redirecting The Propeller Slipstream

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Author : Louis P. Tosti
language : en
Publisher:
Release Date : 1955

Hovering Flight Tests Of A Four Engine Transport Vertical Take Off Airplane Model Utilizing A Large Flap And Extensible Vanes For Redirecting The Propeller Slipstream written by Louis P. Tosti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Airplanes categories.

An investigation of the take-off, landing, and hovering-flight characteristics of a four-engine-transport, vertical take-off airplane has been conducted with a remotely controlled free-flight model. The model had four propellers distributed along the wing with thrust axes parallel to the fuselage axis. In order to produce direct lift for hovering flight, the propeller slipstream was deflected downward about 70 degrees by a full-span 65-percent-chord flap deflected 90 degrees and eight extensible vanes arranged above the wing in a cascade relation.

Mechanical Properties At Room Temperature Of Four Cermets Of Titanium Carbide With Nickel Binder

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Author : Aldie E. Johnson
language : en
Publisher:
Release Date : 1954

Mechanical Properties At Room Temperature Of Four Cermets Of Titanium Carbide With Nickel Binder written by Aldie E. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Binders (Materials) categories.

Room-temperature stress-strain curves are presented for compression, tension, and shear loadings of four compositions of titanium carbide with nickel binder. Values of ultimate strength, modulus of elasticity, modulus of rigidity, Poisson's ratio in the elastic region, density, and hardness for the four materials are tabulated.

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.

Analytical Investigation Of Acceleration Restrictiion In A Fighter Airplane With An Automatic Control System

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Author : James T. Matthews
language : en
Publisher:
Release Date : 1958

Analytical Investigation Of Acceleration Restrictiion In A Fighter Airplane With An Automatic Control System written by James T. Matthews and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Acceleration (Mechanics) categories.

A theoretical analysis was made to investigate the performance and acceleration-restriction capabilities of a normal-acceleration command control system in a fighter airplane. Several combinations of pitching velocity and pitching acceleration were investigated as feedback quantities in combination with normal acceleration.

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.

Report

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Author :
language : en
Publisher:
Release Date : 1958

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 1958 with Aeronautics categories.