An integrated time-varying Airwake in a UH-60 black hawk shipboard landing simulation

AIAA Modeling and Simulation Technologies Conference and Exhibit

Volumn , Issue , 2001, Pages

  Bunnell, John W ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS;

BLADE ELEMENTS; COMPUTATIONAL FLUID DYNAMICS TECHNIQUE; INTEGRATED SIMULATIONS; LANDING SIMULATIONS; RESEARCH CENTER; SHIP AIRWAKES; TURBULENT FIELDS; VERTICAL MOTION SIMULATORS;

SHIPS;

EID: 85086615291     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4065     Document Type: Conference Paper

References (3)

1. Howlett, J.J., "UH-60A Black Hawk Engineering Simulation Program: Volume I - Mathematical Model," NASA CR-166309, United Technologies, Sikorski Aircraft, Stratford, CT, December 1981.
2. Polsky, S., and Bruner, C., "Time-Accurate Computational Simulations of an LHA Ship Airwake", AIAA-2000-4126, August, 2000.
3. Tischler, M.B., and Cauffman, M.G., Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics, Journal of the American Helicopter Society, Vol. 37, No. 3, pp. 3-17, July 1992.