Wind Tunnel Investigation Of The Aerodynamic And Structural Deflection Characteristics Of The Goodyear Inflatoplane PDF Download

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Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane

Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane
Author: Bennie W. Cocke (Jr.)
Publisher:
Total Pages: 62
Release: 1958
Genre: Aerodynamic load
ISBN:

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Summary: An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane over a range of test velocities from minimum stall speed up to speeds giving load factors for wing buckling. Tests were conducted over a range of speeds from approximately 41 to 70 mph with wing-guy-cable loads, wing-distortion photographs, and aerodynamic-force data recorded at each speed for a full range of angle of attack.


Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane

Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane
Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
Total Pages: 62
Release: 2021-09-10
Genre:
ISBN: 9781015219618

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This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.


The Inflatoplane

The Inflatoplane
Author: Bennie W. Cocke
Publisher:
Total Pages: 56
Release: 1958
Genre: Inflatoplane (Airplane)
ISBN:

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The Inflatoplane

The Inflatoplane
Author: Bennie W. Cocke
Publisher:
Total Pages: 56
Release: 1958
Genre: Inflatoplane (Airplane)
ISBN:

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NACA Research Memorandum

NACA Research Memorandum
Author: Bennie W. Cocke (Jr.)
Publisher:
Total Pages: 64
Release: 19??
Genre: Aerodynamics
ISBN:

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Summary: An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane over a range of test velocities from minimum stall speed up to speeds giving load factors for wing buckling. Tests were conducted over a range of speeds from approximately 41 to 70 mph with wing-guy-cable loads, wing-distortion photographs, and aerodynamic-force data recorded at each speed for a full range of angle of attack.


Wind-tunnel Investigation of the Aerodynamic and Structural-deflection Characteristics of an Inflatable Airplane

Wind-tunnel Investigation of the Aerodynamic and Structural-deflection Characteristics of an Inflatable Airplane
Author: H. C. Mc Lemore
Publisher:
Total Pages: 208
Release: 1962
Genre: Airplanes
ISBN:

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Tests were conducted in the Langley full-scale tunnel for a range of speeds from minimum stall speed to speeds at which it was possible to produce a load factor sufficient to cause wing buckling. Static aerodynamic and control data, wing-pressure-distribution data, wing-deflection photographs, and wing-guy-cable loads are presented. Results of the tests show that a maximum load factor of the order of 4.50 can be attained for a normal inflation pressure of 7.0 lb/sq in.


Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 388
Release: 1959
Genre: Aeronautics
ISBN:

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