Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane PDF full book. Access full book title Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane by Bennie W. Cocke (Jr.). Download full books in PDF and EPUB format.
Author: Bennie W. Cocke (Jr.) Publisher: ISBN: Category : Aerodynamic load Languages : en Pages : 62
Book Description
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.
Author: Bennie W. Cocke (Jr.) Publisher: ISBN: Category : Aerodynamic load Languages : en Pages : 62
Book Description
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.
Author: H. C. Mc Lemore Publisher: ISBN: Category : Airplanes Languages : en Pages : 208
Book Description
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.
Author: Bennie W. Cocke (Jr.) Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 64
Book Description
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.
Author: Bennie W. Cocke (Jr.)
Author: Bennie W. Cocke (Jr.)
Author: H. C. Mc Lemore
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: 
Author: Bennie W. Cocke (Jr.)
Author: 
Author: Defense Documentation Center (U.S.)
Author: United States. National Advisory Committee for Aeronautics