Techniques For Improving The Stability Of Soft Inplane Hingeless Rotors

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NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 84 pages
File Size : 43,8 Mb
Release : 1990
Category : Science
ISBN : STANFORD:36105024798683

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NASA Technical Paper by Anonim Pdf

NASA Technical Paper

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 380 pages
File Size : 53,9 Mb
Release : 1990
Category : Aeronautics
ISBN : UOM:39015022359130

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NASA Technical Paper by United States. National Aeronautics and Space Administration Pdf

Helicopter Theory

Author : Wayne Johnson
Publisher : Courier Corporation
Page : 1122 pages
File Size : 40,6 Mb
Release : 2012-03-07
Category : Technology & Engineering
ISBN : 9780486131825

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Helicopter Theory by Wayne Johnson Pdf

Monumental engineering text covers vertical flight, forward flight, performance, mathematics of rotating systems, rotary wing dynamics and aerodynamics, aeroelasticity, stability and control, stall, noise, and more. 189 illustrations. 1980 edition.

Aeromechanical Stability of a Hingeless Rotor in Hover and Forward Flight: Analysis and Wind Tunnel Tests

Author : Anonim
Publisher : Unknown
Page : 24 pages
File Size : 46,8 Mb
Release : 1983
Category : Electronic
ISBN : NASA:31769000560055

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Aeromechanical Stability of a Hingeless Rotor in Hover and Forward Flight: Analysis and Wind Tunnel Tests by Anonim Pdf

A research effort of analysis and testing has been conducted in the NASA-Langley Transonic Dynamics Tunnel to investigate the ground resonance phenomenon of a soft in-plane hingeless rotor. Experimental data were obtained using a 9 ft. (2.74 m) diameter model rotor in hover and forward flight. Eight model rotor configurations were investigated. Configuration parameters included pitch-flap coupling, blade sweep and droop, and precone of the blade feathering axis. An analysis based on a comprehensive analytical model of rotorcraft aerodynamics and dynamics was used for this study. The moving-block method was used to experimentally determine the regressing lead-lag mode damping. Good agreement has been obtained between the analysis and test. Both analysis and experiment indicated ground resonance instability in hover. The paper presents an outline of the analysis, a description of the experimental model and procedures, and comparison of the analytical and experimental data. (Author).

NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 446 pages
File Size : 42,5 Mb
Release : 1977
Category : Electronic
ISBN : MINN:31951000846597E

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NASA Technical Note by Anonim Pdf

Vertica

Author : Anonim
Publisher : Unknown
Page : 636 pages
File Size : 40,9 Mb
Release : 1990
Category : Helicopters
ISBN : UOM:39015026552300

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Vertica by Anonim Pdf

Journal of the American Helicopter Society

Author : American Helicopter Society
Publisher : Unknown
Page : 332 pages
File Size : 47,7 Mb
Release : 2000
Category : Helicopters
ISBN : UVA:X006157665

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Journal of the American Helicopter Society by American Helicopter Society Pdf

Aeromechanical Stability of a Hingeless Rotor in Hover and Forward Flight

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 24 pages
File Size : 49,5 Mb
Release : 2018-07-21
Category : Electronic
ISBN : 172344202X

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Aeromechanical Stability of a Hingeless Rotor in Hover and Forward Flight by National Aeronautics and Space Administration (NASA) Pdf

A research effort of analysis and testing was conducted to investigate the ground resonance phenomenon of a soft in-plane hingeless rotor. Experimental data were obtained using a 9 ft. (2.74 m) diameter model rotor in hover and forward flight. Eight model rotor configurations were investigated. Configuration parameters included pitch flap coupling, blade sweep and droop, and precone of the blade feathering axis. An analysis based on a comprehensive analytical model of rotorcraft aerodynamics and dynamics was used. The moving block was used to experimentally determine the regressing lead lag mode damping. Good agreement was obtained between the analysis and test. Both analysis and experiment indicated ground resonance instability in hover. An outline of the analysis, a description of the experimental model and procedures, and comparison of the analytical and experimental data are presented. Yeager, W. T., Jr. and Hamouda, M. N. H. and Mantay, W. R. Langley Research Center NASA-TM-85683, NAS 1.15:85683, AVRADCOM-TR-83-B-5, AD-A134612 DA PROJ. 1L2-62209-AH-76; RTOP 505-42-23-05

Aeronautical Engineering

Author : Anonim
Publisher : Unknown
Page : 722 pages
File Size : 52,5 Mb
Release : 1993
Category : Aeronautics
ISBN : STANFORD:36105012119983

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Aeronautical Engineering by Anonim Pdf

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)