Analysis on the Power Characteristics of Lift-Fan VTOL

Author:

Zheng Zhi Cheng1,Zhu Xiao Ping1,Chang Min1,Zhou Zhou1

Affiliation:

1. Northwestern Polytechnical University

Abstract

Based on the propeller momentum theory, this paper obtained the momentum model for internal flow of lift fan system. It analyzed the influence of its conceptual parameters on power characteristics of lift-fan VTOL to analyze the trend changes of the total power required with the increase of freestream velocity. The results can be used for selecting parameters at the preliminary phase of designing lift-fan VTOL and determining the design parameters of lift-fan VTOL.

Publisher

Trans Tech Publications, Ltd.

Reference9 articles.

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2. AIAA VTOL Systems Committee, VTOL-1968, AIAA-44054-169, (1969).

3. LIU PeiQing: Air propeller theory and its applications, Beijing Aeronautics and Astronautics Press, 2005: 55-65 (in Chinese).

4. Wang Shicun,Helicopter Aerodynamics,Group of aviation professionals needed teaching materials,1985. 1. (in Chinese).

5. LI Jianbo, GAO Zheng. Experimental Investigation on Lift and Drag of Ducted Fan System, Journal of Nanjing University of Aeronautics & Astronautics, 2004, 36(2): 164-168.

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