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Alford, William J., Jr.: Some Effects of Horizontal-Tail Position on the Vertical-Tail Pressure Distributions of a Complete Model in Sideslip at High Subsonic Speeds. NASA Memo. 10-5-58L, 1958

 Item — Box: 2, Folder: 2

Scope and Content

From the Collection:

The collection contains NACA and NASA research memoranda and reports, publication drafts, research notes and patent details for the variable-sweep wing design, correspondence, award certificates, AIAA (American Institute of Aeronautics & Astronautics) conference programs, and personnel file papers pertaining to William J. Alford's career as an aeronautical engineer. Also included are a Langley working paper, with associated variable-sweep research notes and patent details, and a detailed schematic drawing, of "the variable sweep wing configuration tested in the high-speed 7- by 10- foot tunnel." These materials date from 1951 to 1988.

Some related materials may appear in separate folders. For example, awards and correspondence are also included in the biographical and career information file. Additionally, some personnel file papers, especially many of those in the biographical and career information file, contain photocopies in the place of the original documents.

Dates

  • Other: 1958

Creator

Language of Materials

From the Collection:

The materials in the collection are in English.

Conditions Governing Access

The collection is open for research.

Extent

From the Collection: 0.6 Cubic Feet (2 boxes)

Repository Details

Part of the Special Collections and University Archives, Virginia Tech Repository

Contact:
Special Collections and University Archives, University Libraries (0434)
560 Drillfield Drive
Newman Library, Virginia Tech
Blacksburg Virginia 24061 US
540-231-6308