Sizing methodology for reaction-driven, stopped-rotor vertical takeoff and landing concepts
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287-6106
2. McDonnell Douglas Helicopter Company, Mesa, Arizona 85215
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46887
Reference21 articles.
1. 'Head, R. E. "Reaction Drive Rotors-Lessons Learned (Hero Had a Good Idea-But!),1' AIAA Paper 92-4279, Aug. 1992.
2. 4Wilkerson, J. B., Schneider, J. J., and Bartie, K. M. "Technology Needs for High-Speed Rotorcraft (I),11NASA CR-177585, May 1991.
3. 5Scott, M. W. "Technology Needs for High-Speed Rotorcraft (2),11NASA CR-177590, Aug. 1991.
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