Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis
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Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis

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Published by National Aeronautics and Space Administration, Ames Research Center, National Technical Information Service, distributor in Moffett Field, Calif, [Springfield, Va .
Written in English

Subjects:

  • Rotors (Helicopters) -- Aerodynamics.

Book details:

Edition Notes

StatementTodd R. Quackenbush ... [et al].
SeriesNASA contractor report -- 177611., NASA contractor report -- NASA CR-177611.
ContributionsQuackenbush, Todd R., Ames Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL14690770M

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An Analysis of Harmonic Airloads Acting on Helicopter Rotor Blades. A helicopter rotor in forward flight is subjected to a complex system of loads, both aerodynamic and inertial in origin. A full-span free-wake method is coupled with an unsteady panel method to accurately predict the unsteady aerodynamics of helicopter rotor blades in hover and forward flight. The unsteady potential-based panel method is used to consider aerodynamics of finite thickness multi-bladed rotors, and the full-span free-wake method is applied to Cited by: 5. A 'read' is counted each time someone views a publication summary (such as the title, abstract, and list of authors), clicks on a figure, or views or downloads the full-text. Wachspress, H. Alexander Boschitsch and Kiat Chua(), Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis, NASA-CR, pp. Jan

Tiltrotor aerodynamic interaction, especially in the transition mode, is a necessary consideration for tiltrotor aerodynamics, and structural design and optimization. Previous studies have paid much attention to the helicopter mode. However, due to the substantial complexity of the problem, only a small amount of work on the transition mode has been done so far. In this paper, the rotor&ndash Author: Zhenlong Wu, Can Li, Yihua Cao. Reference-free in-flight BOS to visualise the rotor tip vortices and wake (Left) Retroreflective synthetic dot background, from Ref. [] (Right) natural stone background, from Ref. [ Leading scientists, researchers and inventors describe the findings and innovations accomplished in current research programs and industry applications throughout the world. Topics included cover a wide range of new aerodynamics concepts and their applications for real world fixed-wing (airplanes), rotary wing (helicopter) and quad-rotor aircraft. Full text of "NASA Technical Reports Server (NTRS) Research and technology, " See other formats.

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