Skip to main content

Airplanes -- Design and construction -- Research

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

Found in 125 Collections and/or Records:

"Covering Wing Gasoline Tanks in Martin Bomber" (Air Service Information Circular (Heavier-Than-Air) Vol. II, No. 105), 1920-07-15, 1920-08-20

 Item — Box MC-019-001, Folder: 001.A.009
Identifier: 20141105
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Heavier-than-Air) Vol. II, No. 105 (dated August 20, 1920.

Scope: Report prepared by Engineering Division, Air Service, McCook Field.

Contents: See title.

Dates: 1920-07-15; Publication: 1920-08-20
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

"Design and Testing of Wing Ribs" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. I, No. 4), 1918-09

 Item — Box MC-019-001, Folder: 001.A.004
Identifier: 20140704
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. I, No. 4 (dated September 1918). This section on pages 5 through 25.Scope: By Aeronautical Research Section. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Methods of Conducting...
Dates: Publication: 1918-09
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

"Determination of the Best Wing Loading for Single-Seater Pursuit Airplane" (Air Service Information Circular (Aviation) Vol. IV, No. 315), 1921-08-18, 1922-03-15

 Item — Box MC-019-001, Folder: 001.A.012
Identifier: 20141318
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 315 (dated March 15, 1922), based on McCook Field Report Serial No. 1740 (dated August 18, 1921).

Scope: Report prepared by Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.

Contents: See title."

Dates: 1921-08-18; Publication: 1922-03-15
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

"Effect of Tilt of the Propeller Axis on the Longitudinal-Stability Characteristics of Single-Engine Airplanes" (NACA Report No. 774), 1944

 Item — Box MC-019-001, Folder: 001.A.025
Identifier: 20060142
Scope and Contents

Document Type: Technical Research Report Authority: Government Civil (authoritative reference) Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 774, published in 1944.

Scope: NACA research report by Harry J. Goett and Noel K. Delany.

Contents: See title.

Dates: Publication: 1944
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

"Effect on Variation in Load Factor on Structral Weight of WIngs" (Air Service Information Circular (Aviation) Vol. IV, No. 318), 1921-09-13, 1922-03-15

 Item — Box MC-019-001, Folder: 001.A.012
Identifier: 20141322
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 318 (dated March 15, 1922), based on McCook Field Report Serial No. 1749 (dated September 13, 1921).

Scope: Report prepared by Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.

Contents: See title."

Dates: 1921-09-13; Publication: 1922-03-15
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

"Effects of Canopy Shape on Low-Speed Aerodynamic Characteristics of a 55 degree Swept Parawing with Large-Diameter Leading Edges" (NASA Technical Note TN D-2551), 1964-12

 Item — Box MC-019-002, Folder: 001.A.061
Identifier: 20060057
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2551, dated December 1964.

Scope: Preliminary NASA research report by Delwin R. Croom, Rodger L. Naeseth and William C. Sleeman, Jr. of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1964-12
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

"Effects of Varying Aspect Ratio" (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 Experimental Department, Airplane Engineering Division, U.S.A. [United States Army], Vol. I, No. 3 (dated August 1918. This section on pages 51 through 54.Scope: Based on "Aeronautical Research Department Report." Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Recent...
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

"Evaluation of High-Angle-Of-Attack Aerodynamic-Derivative Data and Stall-Flutter Prediction Techniques" (NACA Technical Note 2533), 1951-11

 Item — Box MC-019-001, Folder: 001.A.035
Identifier: 20060114
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 2533, dated November 1951.

Scope: Preliminary NACA research report by Robert L. Halfman, H. C. Johnson and S. M. Haley of the Massachusetts Institute of Technology under NACA contract.

Contents: See title.

Dates: Publication: 1951-11
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 Aerodynamic Derivatives of a Sinusoidally Oscillating Air-Foil in Two-Dimensional Flow" (NACA Report 1108), 1952

 Item — Box MC-019-001, Folder: 001.A.028
Identifier: 20060153
Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1108, published in 1952.

Scope: NACA research report by Robert L. Halfman of the Massachusetts Institute of Technology under NACA contract.

Contents: See title.

Dates: Publication: 1952
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

Staff Interface | Visit ArchivesSpace.org | v3.5.0