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Airplanes -- Design and construction -- Research

 Subject
Subject Source: World Cat Fast Authority File
Scope Note: For basic aerodynamics work, use "Aerodynamics".

Found in 94 Collections and/or Records:

"Veneer Fuselage Construction, Part 2" (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 5 through 26.Scope: By the Experimental Department. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Manufacture of Veneer and...
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

"Wind-Tunnel Investigation of Effect of Interference on Lateral-Stability Characteristics of Four NACA 23012 Wings an Elliptical and A Circular Fuselage and Vertical Fins" (NACA Report No. 705), 1941

 Item — Box MC-019-001, Folder: 001.A.025
Identifier: 20060137
Scope and Contents

Document Type: Technical Research Report Authority: Government Civil (authoritative reference) Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 705, published in 1941.

Scope: NACA research report by Rufus O. House and Arthur R. Wallace.

Contents: See title.

Dates: Publication: 1941
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

"Wind Tunnel Test of the Original TA-4 with the Following Airfoils: USA-27C Large; USA-27C Small; Gottingen 387; Gottingen 255" (Air Service Information Circular (Aviation) Vol. V, No. 455), 1923-11-22, 1924-03-15

 Item — Box MC-019-001, Folder: 001.A.017
Identifier: 20141460
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Aviation) Vol. V, No. 455 (dated March 15, 1924), based on McCook Field Report Serial No. 2259 (dated November 22, 1923).

Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.

Contents: See title.

Dates: 1923-11-22; Publication: 1924-03-15
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

"Wind Tunnel Test of the Original TA-4 with the Following Airfoils: USA-27C Large; USA-27C Small; Gottingen 387; Gottingen 255" (Air Service Information Circular (Aviation) Vol. V, No. 455), 1923-11-22, 1924-03-15

 Item — Box MC-019-001, Folder: 001.A.019
Identifier: 20200076
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Aviation) Vol. V, No. 455 (dated March 15, 1924), based on McCook Field Report Serial No. 2259 (dated November 22, 1923).

Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.

Contents: See title.

Dates: 1923-11-22; Publication: 1924-03-15
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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