Elevated-temperature Compressive Stress-strain Data for 24S-T3 Aluminum-alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy

Elevated-temperature Compressive Stress-strain Data for 24S-T3 Aluminum-alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy PDF Author: William M. Roberts
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 18

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Book Description
Results are presented of compressive stress-strain tests of 24S-T3 aluminum-alloy sheet at stabilized elevated temperatures up to 700 degrees F, exposure times of 1/2 to 2 hours, and strain rates of 0.002 to 0.006 per minute. Some general comparisons with extruded 75S-T6 aluminum alloy are included.

Elevated-temperature Compressive Stress-strain Data for 24S-T3 Aluminum-alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy

Elevated-temperature Compressive Stress-strain Data for 24S-T3 Aluminum-alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy PDF Author: William M. Roberts
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 18

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Book Description
Results are presented of compressive stress-strain tests of 24S-T3 aluminum-alloy sheet at stabilized elevated temperatures up to 700 degrees F, exposure times of 1/2 to 2 hours, and strain rates of 0.002 to 0.006 per minute. Some general comparisons with extruded 75S-T6 aluminum alloy are included.

Tests of Two-blade Propellers in the Langley 8-foot High-speed Tunnel to Determine the Effect on Propeller Performance of a Modification of Inboard Pitch Distribution

Tests of Two-blade Propellers in the Langley 8-foot High-speed Tunnel to Determine the Effect on Propeller Performance of a Modification of Inboard Pitch Distribution PDF Author: James Benjamin Delano
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ISBN:
Category : Propellers, Aerial
Languages : en
Pages : 724

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Book Description
This paper presents propeller characteristics for two propellers that differ only in inboard pitch distribution. The forward Mach number range extended to 0.062 and the blade-angle range was from 20 to 55 degrees. Section thrust-coefficient data are also presented to afford a more detailed analysis of the effects of modifying the pitch distribution of the inboard sections of a propeller.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1208

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Technical Note

Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 624

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 412

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 692

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Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.

Hearings

Hearings PDF Author: United States. Congress Senate
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ISBN:
Category :
Languages : en
Pages : 2862

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Stockpile and Accessibility of Strategic and Critical Materials to the United States in Time of War: Titanium

Stockpile and Accessibility of Strategic and Critical Materials to the United States in Time of War: Titanium PDF Author: United States. Congress. Senate. Committee on Interior and Insular Affairs
Publisher:
ISBN:
Category : Strategic materials
Languages : en
Pages : 856

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