by National Aeronautics and Space Administration, Ames Research Center, US Army Aviation Systems Command, Aviation Research and Technology Activity in Moffett Field, Calif .
Written in English
|Other titles||Modeling methods for high fidelity rotorcraft flight mechanics simulation|
|Statement||M. Hossein Mansur ... [et al.].|
|Series||NASA technical memorandum -- 103842, USAAVSCOM technical report -- 91-A-005, AVSCOM technical report -- 91-A-5.|
|Contributions||Mansur, M. Hossein., Ames Research Center., United States. Army Aviation Research and Technology Activity.|
|The Physical Object|
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Modeling the Aerodynamic Interaction of Multiple Rotor Vehicles and Compound Rotorcraft with Viscous Vortex Particle Method. This paper presents an efficient and high fidelity aerodynamic interaction modeling method for effective simulation and analysis of compound rotorcraft as well as aircraft configured with multiple rotors. The Cited by: 2. FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT NI*, I*, **, NI** *AgustaWestland, Varese, Italy, ** University of Bologna, Italy Keywords: Flight Dynamics and Control - Flight Testing and Simulation – Simulator design Abstract This paper describes the design and. rotorcraft noise prediction and flight dynamics simulation into a real-time or near real-time analysis code. The high-fidelity noise prediction code PSU-WOPWOP3,4 (also known as WOPWOP3) has been mated with the flight simulation model GENHEL1 to provide a flight dynamics and acoustics analysis of a utility transport helicopter. An analytic modeling and system identification study of rotor/fuselage dynamics at hover [microform] / S On the appropriateness of applying chi-square distribution based confidence intervals to spectral estima Modeling methods for high-fidelity rotorcraft flight mechanics simulation [microform] / M. Hossein Mansu.