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Wind tunnel testing

 Subject
Subject Source: Library of Congress Subject Headings
Scope Note: Here are entered works on the testing of objects in wind tunnels to determine the objects' aerodynamic characteristics. Works on the testing of wind tunnels to determine the tunnels' performance characteristics are entered under the heading Wind tunnels--Testing.

Found in 4 Collections and/or Records:

"Analysis of Wind-Tunnel Data on Directional Stability and Control" (NACA Technical Notes No. 775), 1940-09

 Item — Box MC-019-001, Folder: 001.A.030
Identifier: 20060102
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 775, dated September 1940.

Scope: Preliminary NACA research report by H. R. Pass of Langley Memorial Aeronautical Laboratory, Langley Field, Va.

Contents: See title.

Dates: Publication: 1940-09
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

"Low-Speed Wind-Tunnel Investigation of the Effects of Propeller Operation at High Thrust on the Longitudinal Stability and Trim of A Twin-Engine Airplane Configuration" (NACA Research Memorandum L52D04), 1952-07-14

 Item — Box MC-019-002, Folder: 001.A.037
Identifier: 20060162
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Research Memorandum L52D04, dated July 14, 1952. Declassified on December 11, 1953.

Scope: Preliminary classified NACA research report by William C. Sleeman, Jr. and Edward L. Linsley of Langley Aeronautical Laboratory, Langley Field, Va.

Contents: See title.

Dates: Publication: 1952-07-14
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 Effects Of Various Aerodynamic Balance Shapes and Sweepback on Control-Surface Characteristics of Semispan Tail Surfaces With NACA 0009, 0015, 66-009, 66(215)-014, And Circular-ARC Airfoil Sections" (NACA Technical Note 2495), 1951-10

 Item — Box MC-019-001, Folder: 001.A.033
Identifier: 20060112
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 2495, dated October 1951.

Scope: Preliminary NACA research report by John J. Harper of the Georgia Institute of Technology under NACA contract.

Contents: See title.

Dates: Publication: 1951-10
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.A: Aircraft RDT&E

"Wind-Tunnel Tests of A 2-Engine Airplane Model As A Preliminary Study of Flight Conditions Arising On The Failure of One Engine" (NACA Technical Notes No. 646), 1938-04

 Item — Box MC-019-001, Folder: 001.A.030
Identifier: 20060101
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 646, dated April 1938.

Scope: Preliminary NACA research report by Edwin P. Hartman of Langley Memorial Aeronautical Laboratory, Langley Field, Va.

Contents: See title.

Dates: Publication: 1938-04
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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