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Computational analysis of hover performance using a new free wake methodThe development of EHPIC (Evaluation of Hover Performance using Influence Coefficients), a hover performance analysis code incorporating a new free wake analysis method based on the use of influence coefficients, is discussed. The technical principles underlying the EHPIC code are examined with emphasis on the extension of single-filament wake models to a multi-bladed multifilament wake suitable for realistic hover performance predictions. The coupling of the wake model to a lifting surface loads analysis is described, and sample problems are solved to demonstrate the robustness of the method.
Document ID
19880064533
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Quackenbush, Todd R.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Wachspress, Daniel A.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Bliss, Donald B.
(Duke University Durham, NC, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aerodynamics
Meeting Information
Meeting: International Conference on Rotorcraft Basic Research
Location: College Park, MD
Country: United States
Start Date: February 16, 1988
End Date: February 18, 1988
Accession Number
88A51760
Funding Number(s)
CONTRACT_GRANT: NAS2-12148
Distribution Limits
Public
Copyright
Other

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