Forward flight trim and frequency response validation of a helicopter simulation model
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. 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/10.2514/3.46427
Reference22 articles.
1. Validation of the Dynamic Response of a Blade‐Element UH‐60 Simulation Model in Hovering Flight
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