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Propellers, Aerial -- Design and construction

 Subject
Subject Source: World Cat Fast Authority File

Found in 19 Collections and/or Records:

"Propeller Hub Dowel and Key Location" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 3) [Photocopy], 1918-12

 Item — Box MC-019-001, Folder: 001.A.007
Identifier: 20140707
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A. [United States Army], Vol. II, No. 3 (dated December 1918). This section on page 113 (bottom half).Scope: By the Experimental Department. Intended for limited, controlled distribution (see General note on publication data).Contents: drawing showing standardized propeller hub...
Dates: Publication: 1918-12
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

"Propeller Reduction Gears in General" (Bulletin of the Airplane Engineering Department, U.S.A, Vol. I, No. 3), 1918-08

 Item — Box MC-019-001, Folder: 001.A.003
Identifier: 20140703
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Airplane Engineering Department, U.S.A. [United States Army], Vol. I, No. 3 (dated August 1918. This section on pages 78 through 88.Scope: Final Design Department Report. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Discussion of Best Form of Tooth to Use – Various...
Dates: Publication: 1918-08
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

"Protecting Propellers Against Abrasion" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 1), 1918-10

 Item — Box MC-019-001, Folder: 001.A.005
Identifier: 20140705
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A. [United States Army], Vol. II, No. 1 (dated October 1918). This section on pages 83 through 89.Scope: "Technical Publications Section Compilation". Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Methods of...
Dates: Publication: 1918-10
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

Sub-series III.C: Aircraft Engine Components

 Sub-Series
Scope and Contents

Includes engine components (e.g. propellers, magnetos, fuel systems) and auxillary systems.

Dates: 1911 - 2013
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series III: Aircraft Engines (commercial & military)

Thrusting Forward: A History of the Propeller, 1984

 Item — Special collection MC-19, Book: 112, Call No.: TL 705 .R58 1984 Oversized
Identifier: 20135012
Scope and Contents

Document Type: Book (Historical Study). Purpose: Informational. Authority: Author Expertise.

Scope: TBD

Contents: TBD

Dates: Publication: 1984
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series III: Aircraft Engines (commercial & military) / Sub-series III.E: Aircraft Engines (Special Collection)

"Trim Requirements and Static-Stability Derivatives from a Wind-Tunnel Investigation of a Lifting Rotor in Transition" (NASA Technical Note TN D-2655), 1965-02

 Item — Box MC-019-002, Folder: 001.A.062
Identifier: 20060066
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2655, dated February 1965.

Scope: Preliminary NASA research report by Julian L. Jenkins, Jr. of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1965-02
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

United Aircraft Corporation. Hamilton Standard Division (1929-1975)

 Organization

United Technologies Corporation. Hamilton Standard Division (1975-1999)

 Organization

"Wind-Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45" (NASA Technical Note TN D-2628), 1965-02

 Item — Box MC-019-002, Folder: 001.A.062
Identifier: 20060064
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2628, dated February 1965.

Scope: Preliminary NASA research report by Julian L. Jenkins, Jr. of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1965-02
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

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