Optimum Design of a Compound Helicopter
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40101
Reference10 articles.
1. Aeromechanics Analysis of a Heavy Lift Slowed-Rotor Compound Helicopter
2. Performance Analysis of a Utility Helicopter with Standard and Advanced Rotors
3. Assessment of Comprehensive Analysis Calculation of Airloads on Helicopter Rotors
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