Airfoil Section Data Obtained in the N.A.C.A. Variable-density Tunnel as Affected by Support Interference and Other Corrections PDF Download
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Author: Eastman Nixon Jacobs
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
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Book Description
Author: Eastman Nixon Jacobs
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
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Book Description
Author: Eastman N. Jacobs
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1068
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Book Description
Author: William D. Deveikis
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 584
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Book Description
Elevated-temperature compressive-strength test results from room temperature to 600 degrees F and creep test results from 350 degrees F to 500 degrees F are presented for V-groove edge-supported plates of 7075-T6 aluminum alloy. The test data are compared with calculations obtained from procedures for estimating maximum strength from material stress-strain curves and creep-failure stresses from isochronous stress-strain curves. The strength and creep results from this investigation are also compared with similar results from 2024-T3 aluminum-alloy plates.
Author:
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ISBN:
Category : Executive departments
Languages : en
Pages : 666
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Book Description
Contains information on the agencies of the legislative, judicial, and executive branches. Also, includes information on quasi-official agencies, international organizations in which the United States participates, and boards, commissions, and committees.
Author:
Publisher:
ISBN:
Category : Administrative agencies
Languages : en
Pages : 672
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2868
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Book Description
Author: Donald R. Riley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
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Book Description
An investigation has been conducted in the Langley stability tunnel on a vertical-tail model with a stub fuselage in combination with various horizontal tails to determine the effect of horizontal-tail span and vertical location of the horizontal tail relative to the vertical tail on the aerodynamic characteristics of an unswept tail assembly in sideslip.
