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Home > Reference > Research and information: general > Research methods: general > A Comparison of Interactional Aerodynamics Methods for a Helicopter in Low Speed Flight
A Comparison of Interactional Aerodynamics Methods for a Helicopter in Low Speed Flight

A Comparison of Interactional Aerodynamics Methods for a Helicopter in Low Speed Flight


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About the Book

Recent advances in computing subsonic flow have been applied to helicopter configurations with various degrees of success. This paper is a comparison of two specific methods applied to a particularly challenging regime of helicopter flight, very low speeds, where the interaction of the rotor wake and the fuselage are most significant. Comparisons are made between different methods of predicting the interactional aerodynamics associated with a simple generic helicopter configuration. These comparisons are made using fuselage pressure data from a Mach-scaled powered model helicopter with a rotor diameter of approximately 3 meters. The data shown are for an advance ratio of 0.05 with a thrust coefficient of 0.0066. The results of this comparison show that in this type of complex flow both analytical techniques have regions where they are more accurate in matching the experimental data. Berry, John D. and Letnikov, Victor and Bavykina, Irena and Chaffin, Mark S. Unspecified Center NASA/TM-1998-208420, L-17732, NAS 1.15:208420, AFDD/TR-98-A-003 RTOP 581-10-11-01...


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Product Details
  • ISBN-13: 9781724981370
  • Publisher: Createspace Independent Publishing Platform
  • Publisher Imprint: Createspace Independent Publishing Platform
  • Height: 279 mm
  • No of Pages: 32
  • Spine Width: 2 mm
  • Width: 216 mm
  • ISBN-10: 1724981374
  • Publisher Date: 09 Aug 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 100 gr


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