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Aircraft Wake Turbulence Controllability Experiment

  • R. P. Johannes
Conference paper

Abstract

The development of extremely large, high gross weight aircraft over the past several years has greatly increased the significance of aircraft wake turbulence. The increased magnitude of this turbulence and its effect on other aircraft is of major concern to the aircraft community. This concern is evidenced by the very fact that this symposium is being held for the purpose of considering the wake turbulence phenomenon and developing methods to cope with its effects. From a practical, operational point of view, perhaps the two most critical areas of concern are the induced structural loads and vehicle upset which can result from wake vortex encounter.

Keywords

Outer Loop Wake Turbulence Roll Rate Pilot Activity Flexible Aircraft 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    AFFDL-TR-68–158, “Aircraft Load Alleviation and Mode Stabilization (LAMS)”, Burris, P. M. and Bender, M. A., April 1968.Google Scholar
  2. 2.
    Boeing Document D3–8100, “Demonstration of the LAMS-FCS in the Wake of a C-141”,, August 1969.Google Scholar
  3. 3.
    Boeing Document D3–8357, “C-141 Wake Turbulence Evaluation”, May 1970.Google Scholar

Copyright information

© Plenum Press, New York 1971

Authors and Affiliations

  • R. P. Johannes
    • 1
  1. 1.Air Force Flight Dynamics LaboratoryWright-Patterson Air Force BaseUSA

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