Wing force and surface pressure data from a hover test of a 0.658-scale V-22 rotor and wing



Publisher: National Aeronautics and Space Administration, Ames Research Center, Publisher: National Technical Information Service [distributor in Moffett Field, Calif, [Springfield, Va.?

Written in English
Published: Downloads: 536
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Subjects:

  • Rotors -- Testing.

Edition Notes

StatementFort F. Felker ... [et al].
SeriesNASA technical memorandum -- 102244.
ContributionsFelker, Fort F., Ames Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15363428M

Wing force and surface pressure data from a hover test of a 0.658-scale V-22 rotor and wing Download PDF EPUB FB2

WING FORCE AND SURFACE PRESSURE DATA FROM A HOVER TEST OF A SCALE V ROTOR AND WING Fort F. Felker, Patrick R. Shinoda, Ruth M. Heffernan, and Hugh F.

Sheehy* Ames Research Center SUMMARY A hover test of a scale V rotor and wing was conducted in the by Foot Wind Tunnel at Ames Research Size: 8MB. Get this from a library. Wing force and surface pressure data from a hover test of a scale V rotor and wing. [Fort F Felker; Ames Research Center.;].

Wing force and surface pressure data from a hover test of a scale V rotor and wing eBook: NASA, National Aeronautics and Space Administration: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA.

Buy Wing force and surface pressure data from a hover test of a scale V rotor and wing (SuDoc NAS ) by NASA (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : NASA. Modeling the wing in ANSYS Mechanical APDL using working model parameters and applying the loads accordingly.

The idealization of the wing and all. A test of a scale V rotor and wing was conducted in the 40 x 80 Foot Wind Tunnel at Ames Research Center. One of the principal objectives of the test. Wing force and surface pressure data from a hover test of a scale V rotor and wing [microform] Performance and loads data from a hover test of a scale V rotor and wing [microform] / Fort F.

Performance and loads data from a hover test of a full-scale advanced technology XV rotor [microform]. 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 Author: Zhenlong Wu, Can Li, Yihua Cao.Performance and loads data from a hover test of a full-scale advanced technology XV rotor [microform] / Fort F.

Felker, Larry A. Young and David B. Signor National Aeronautics and Space Administration, Ames Research Center ; For sale by the National Technical Information Service Moffett Field, Calif.: [Springfield, Va. Wikipedia Citation. A scale V rotor and wing was used in the large-scale test.

Wing download, wing surface pressure, rotor performance, and rotor downwash data from the large-scale test are presented. Wing force and surface pressure data from a hover test of a scale V rotor and wing (English Edition) eBook: National Aeronautics and Space Administration NASA: Format: Kindle.

Full text of "A study of the effect of design parameter variation on predicted tilt-rotor aircraft other formats NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS u I i A STUDY OF THE EFFECT OF DESIGN PARAMETER VARIATION ON PREDICTED TILT- -ROTOR AIRCRAFT PERFORMANCE by Mary Cottrell Dunston.

Wing Force and Surface Pressure Data from a Hover Test of a Scale V Rotor and Wing Fort F. Felker, Patrick R. Shinoda, Ruth M Heffernan, and Hugh F. Sheehy V22 – Osprey guide book. SCOPUS Indexed Journal [email protected] Hover.

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Full text of "NASA Technical Reports Server (NTRS) Research and technology, " See other formats. Wing force and surface pressure data from a hover test of a scale V rotor and wing.

NASA Technical Reports Server (NTRS) Felker, Fort F.; Shinoda, Patrick R.; Heffernan, Ruth M.; Sheehy, Hugh F. A hover test of a scale V. Fabrication of the replica templated from butterfly wing scales with complex light trapping structures.

NASA Astrophysics Data System (ADS) Han, Zhiwu; Li, Bo; Mu, Zhengzhi; Yang. Figure 8 Surface pressure distribution for a lifting rotor in hover. M t i p = 0. 44, collective pitch 8, Re = 10 6 for the experimental data of Caradonna and Tung ().

(a) From Wake and Sankar () using Navier-Stokes. (b) From Srinivasan and McCroskey () for thin-layer Navier-Stokes; the solid line is the computation.