Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff /
W. Thomas Bundick.

APA Citation

Bundick, W. Thomas., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. (1982). Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch .

MLA Citation

Bundick, W. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. Effects of Cable Geometry And Aircraft Attitude On the Accuracy of a Magnetic Leader Cable System for Aircraft Guidance During Rollout And Turnoff. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch , 1982.

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