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NASA NTRS · Technical Memorandum (TM)

Spin-Tunnel Investigation of a 1/40-Scale Model of the F-111A Airplane with Store Loadings and with Supplementary Spin-Recovery Devices

Published 2000-03-10 From Langley Research Center 2 authors
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Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Langley Research Center.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

An investigation has been made in the Langley spin tunnel to determine the spin and spin-recovery characteristics of the F-111A airplane in the symmetric and asymmetric stores loading conditions. Tests were also made with the model in the clean condition to determine whether the spin-recovery characteristics could be improved by the use of supplementary devices.

Authors

  • James S Bowman, Jr Langley Research Center
  • William L White Langley Research Center

Keywords

  • Spin-recovery parachute
  • Store loadings
  • Spinning

Citation: James S Bowman, Jr, William L White (2000). Spin-Tunnel Investigation of a 1/40-Scale Model of the F-111A Airplane with Store Loadings and with Supplementary Spin-Recovery Devices. Langley Research Center. NASA NTRS ID 20000021277. https://ntrs.nasa.gov/citations/20000021277 ↗