The influence of helicopter rotor-fuselage flow interaction on temperature fields in forward flight

Author:

Li Yanqing,Zhang Jun,Xuan Yimin

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference37 articles.

1. C.E. Freeman, Development and Validation of a Combined Rotor-Fuselage Induced Flow-Field Computational Method, in: DTIC Document, 1980.

2. An unsteady helicopter rotor-fuselage aerodynamic interaction analysis;Lorber;J. Am. Helicop. Soc.,1990

3. T. Renaud, D. O’Brein, M. Smith, M. Potsdam, Evaluation of isolated fuselage and rotor-fuselage interaction using CFD, 2004.

4. Helicopter stabilizer optimization considering rotor downwash in forward-flight;Minervino;Aircraft Eng. Aerosp. Technol.,2016

5. V. Gupta, J.D. Baeder, Investigation of Quad Tiltrotor Aerodynamics in Forward Flight Using CFD, AIAA paper, 2812, 2002.

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