Aerodynamic Characteristics Temperature And Noise Measurements Of A Large Scale External Flow Jet Augmented Flap Model With Turbojet Engines Operating


Aerodynamic Characteristics Temperature And Noise Measurements Of A Large Scale External Flow Jet Augmented Flap Model With Turbojet Engines Operating
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Aerodynamic Characteristics Temperature And Noise Measurements Of A Large Scale External Flow Jet Augmented Flap Model With Turbojet Engines Operating


Aerodynamic Characteristics Temperature And Noise Measurements Of A Large Scale External Flow Jet Augmented Flap Model With Turbojet Engines Operating
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Author : Marvin P. Fink
language : en
Publisher:
Release Date : 1961

Aerodynamic Characteristics Temperature And Noise Measurements Of A Large Scale External Flow Jet Augmented Flap Model With Turbojet Engines Operating written by Marvin P. Fink and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Compressed air categories.


An investigation has been conducted in the Langley full-scale tunnel on a large-scale model powered by turbojet engines with flattened rectangular nozzles. The wing had 35° sweep of the leading edge, an aspect ratio of 6.5, a taper ratio of 0.31, and NACA 65(1)-412 and 65-408 airfoils at the root and tip. The investigation included measurements of the longitudinal aerodynamic characteristics of the model with half-span and full-span flaps and measurements of the sound pressure and skin temperature on the portions of the lower surface of the wing immersed in the jet flow. The tests were conducted over a range or angles of attack from -8° to 16° for Reynolds numbers from 1.8 x 106 to 4.4 x 106 and a range of momentum coefficients from 0 to 2.0. In general, the aerodynamic results of this investigation made with a large-scale hot-jet model verified the results of previous investigations with small models powered by compressed-air jets. Although blowing was only done over the inboard portion of the wing, substantial amounts of induced lift were also obtained over the outboard portion of the wing. Skin temperatures were about 340° F and wing heating could be handled with available materials without cooling. Random acoustic loadings on the wing surface were high enough to indicate that fatigue failure from this source would require special consideration in the design of an external-flow jet flap system for an airplane.



Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1971

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 1971 with categories.




Large Scale Wind Tunnel Investigation Of A Model With An External Jet Augmented Flap


Large Scale Wind Tunnel Investigation Of A Model With An External Jet Augmented Flap
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Author : Jerry V. Kirk
language : en
Publisher:
Release Date : 1967

Large Scale Wind Tunnel Investigation Of A Model With An External Jet Augmented Flap written by Jerry V. Kirk and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aerodynamics categories.




Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1962

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Mechanics, Applied categories.




Static And Dynamic Stability Derivatives Of A Model Of A Jet Transport Equipped With External Flow Jet Augmented Flaps


Static And Dynamic Stability Derivatives Of A Model Of A Jet Transport Equipped With External Flow Jet Augmented Flaps
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Author : Delma C. Freeman
language : en
Publisher:
Release Date : 1969

Static And Dynamic Stability Derivatives Of A Model Of A Jet Transport Equipped With External Flow Jet Augmented Flaps written by Delma C. Freeman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Damping (Mechanics) categories.


Static and dynamic stability derivatives of model jet transport equipped with external flow jet augmented flaps.



U S Government Research Reports


U S Government Research Reports
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Author :
language : en
Publisher:
Release Date : 1961

U S Government Research Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Science categories.




Technical Abstract Bulletin


Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1961-10

Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961-10 with Military art and science categories.




Index To Nasa Technical Publications


Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.




Monthly Catalog Of United States Government Publications


Monthly Catalog Of United States Government Publications
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Author :
language : en
Publisher:
Release Date : 1967

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Government publications categories.




Index Of N A S A Technical Publications


Index Of N A S A Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960

Index Of N A S A Technical Publications written by United States. National Aeronautics and Space Administration 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.