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Variable Sweep Wing Patents & Research. E. Polhamus.

 File — Box: 1, Folder: 1

Scope and Content

From the Collection:

The Edward C. Polhamus Papers include reprints of articles and reports by Polhamus, correspondence, notebooks, and photographs relating to his patents on variable wing sweeps, F-111 aircraft and cryogenic wind tunnel development and vortex lift aerodynamics, Congressional testimony on the TFX contract investigation, and materials relating to his Wright Brothers lectureship.

Dates

  • 1962 - 1986

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: 0.4 Cubic Feet (1 box)

Bibliography

  • E.C. Polhamus. Variable Sweep Aircraft Wing Patent. 17 September 1963.
  • W.J. Alford, Jr. and E.C. Polhamus. Variable Sweep Wing Configuration. 11 September 1962.
  • E.C. Polhamus et al. Variable Sweep Aircraft Patent. 6 September 1966.
  • Ann Ewing. Supersonic Airplane with Changing Wing Patented. 9 September 1962.
  • Donald D. Baals & Edward C. Polhamus. Variable-Sweep Aircraft-Past, Present, and Future. June 1963.
  • NATO. Aiken, W.S. Aiken, Jr., Polhamus, E.C., & Toll, T.A. NASA Variable Research Geometry. April 1963.
  • NASA. Edward C. Polhamus & Thomas A. Toll. Research Related to Variable Sweep Aircraft Development. May 1981.
  • NASA. Alford, William J. Jr., Foster, Gerald V., Polhamus, Edward C. Technical Memorandum. December 1962.
  • Journal of Aircraft. E.C. Polhamus. Applying Slender Wing Benefits to Military Aircraft. August 1984.

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