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Aircraft Engine Historical Society, Inc.

 Organization

Found in 593 Collections and/or Records:

Experimental Aerodynamics, 1940

 Item — Special collection MC-19, Book: 037, Call No.: TL 566 .P3
Identifier: 20061109
Scope and Contents

Document Type: Textbook (Technical). Purpose: Training & Education. Authority: Author Expertise.

Scope: TBD

Contents: TBD

Dates: Copyright: 1940
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.E: Aeronautical RDT&E (Special Collection)

"Experimental and Analytical Investigation of Propeller Whirl Flutter of a Power Plant on a Flexible Wing" (NASA Technical Note TN D-2399), 1964-08

 Item — Box MC-019-002, Folder: 001.A.057
Identifier: 20060047
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2399, dated August 1964.

Scope: Preliminary NASA research report by Robert M. Bennett and Samuel R. Bland of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1964-08
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.A: Aircraft RDT&E

"Experimental Investigation of the Dynamic Stability of a Towed Parawing Glider Air Cargo Delivery System" (NASA Technical Note TN D-2292), 1964-08

 Item — Box MC-019-002, Folder: 001.A.056
Identifier: 20060040
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2292, dated August 1964.

Scope: Preliminary NASA research report by Robert E. Shanks of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1964-08
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.A: Aircraft RDT&E

"Experimental Observations of Transient Boiling of Subcooled Water and Alcohol on a Horizontal Surface" (NASA Technical Note TN D-2507), 1965-01

 Item — Box MC-019-002, Folder: 001.A.059
Identifier: 20060053
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2507, dated January 1965.

Scope: Preliminary NASA research report by Robert W. Graham of Lewis Research Center, Cleveland, Ohio.

Contents: See title.

Dates: Publication: 1965-01
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

"Experimental Verification of Two Methods for Computing the Take-Off Ground Run of Propeller-Driven Aircraft" (NACA Technical Note No. 1258), 1947-06

 Item — Box MC-019-001, Folder: 001.A.031
Identifier: 20060106
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 1258, dated June 1947.

Scope: Preliminary NACA research report by Welko E. Gasich of Ames Aeronautical Laboratory, Moffett Field, Calif.

Contents: See title.

Dates: Publication: 1947-06
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

"Experiments on Thick Wing Sections" (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 pages 84 through 106.Scope: By the Experimental Department. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Aerodynamic Investigation of...
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.A: Aircraft RDT&E

"Experiments with Venturi Tubes" (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 67 through 77.Scope: Report "Translated and Summarized by the Technical Publication Department from French Report by A. Toussaint and G. Lepère." Intended for limited, controlled distribution (see General note on publication data)....
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.A: Aircraft RDT&E

Facts about the Wright Turbo Compound, 1956-05

 Item — Box 096, Folder: 001
Identifier: 20210012
Scope and Contents Type: Technical Sales Brochure From the Foreword: The Turbo Compound introduced new concepts of engine economy and performance to the aircraft engine operator. Higher powers are now available without substantial change in cylinder working conditions. With the compound engine these powers have proved practical, and they are achieved with lower specific fuel consumption and without danger of detonation or increased cylinder stress. Furthermore, they are available without...
Dates: Publication: 1956-05
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series III: Aircraft Engines (commercial & military)

Fast Jets: The History of Reheat Development at Derby (Rolls-Royce Heritage Trust Historical Series #5), 2001

 Item — Special collection MC-19, Book: 114, Call No.: TL 709 .E43 2001
Identifier: 20160505
Scope and Contents Document Type: Book (Historical Study). Purpose: Informational. Authority: Author Expertise. Series: Rolls-Royce Heritage Trust Historical Series #5.NB: The Rolls-Royce Heritage Trust and the Sir Henry Royce Memorial Foundation are closely related. From "Rolls-Royce: The Pursuit of Excellence" (1984): "Both organisations share the history of the early days and work closely in harmony. This Historical Series of books was started by the Trust and it is intended that a series shall...
Dates: Publication: 2001
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)

"Fatigue Under Random and Programed Loads" (NASA Technical Note TN D-2629), 1965-02

 Item — Box MC-019-002, Folder: 001.A.062
Identifier: 20060065
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2629, dated February 1965.

Scope: Preliminary NASA research report by Eugene C. Naumann 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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