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Volumn 48, Issue 3, 2003, Pages 186-198

Modeling refinements in simple tiltrotor whirl flutter analyses

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); FREQUENCIES; TORSIONAL STRESS; TURBOMACHINE BLADES;

EID: 0041765120     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.48.186     Document Type: Article
Times cited : (14)

References (14)
  • 1
    • 0042056184 scopus 로고
    • Recent developments in the dynamics of advanced rotor systems
    • March
    • Johnson, W., "Recent Developments in the Dynamics of Advanced Rotor Systems," NASA TM 86669, March 1985.
    • (1985) NASA TM 86669
    • Johnson, W.1
  • 2
    • 26744478715 scopus 로고
    • Analytical model for tilting proprotor aircraft dynamics, including blade torsion and coupled bending modes, and conversion mode operation
    • May
    • Johnson, W., "Analytical Model for Tilting Proprotor Aircraft Dynamics, Including Blade Torsion and Coupled Bending Modes, and Conversion Mode Operation," NASA TM X-62,369, May 1974.
    • (1974) NASA TM X-62,369
    • Johnson, W.1
  • 5
    • 0005868145 scopus 로고
    • Dynamics of tilting proprotor aircraft in cruise flight
    • May
    • Johnson, W., "Dynamics of Tilting Proprotor Aircraft in Cruise Flight," NASA TN D-7677, May 1974.
    • (1974) NASA TN , vol.D-7677
    • Johnson, W.1
  • 7
    • 0023328253 scopus 로고
    • Correlation of test and analysis for the 1/5-scale V-22 aeroelastic model
    • April
    • Popelka, D., Sheffler, M., and Bilger, J., "Correlation of Test and Analysis for the 1/5-Scale V-22 Aeroelastic Model," Journal of the American Helicopter Society, Vol. 32, (2), April 1987, pp. 21-33.
    • (1987) Journal of the American Helicopter Society , vol.32 , Issue.2 , pp. 21-33
    • Popelka, D.1    Sheffler, M.2    Bilger, J.3
  • 9
    • 0042056179 scopus 로고
    • Analytical modeling requirements for tilting proprotor aircraft dynamics
    • July
    • Johnson, W., "Analytical Modeling Requirements for Tilting Proprotor Aircraft Dynamics," NASA TN D-8013, July 1975.
    • (1975) NASA TN , vol.D-8013
    • Johnson, W.1
  • 10
    • 0026679554 scopus 로고
    • Evolution and test history of the V-22 0.2-scale aeroelastic model
    • January
    • Settle, T. B., and Kidd, D. L., "Evolution and Test History of the V-22 0.2-Scale Aeroelastic Model," Journal of the American Helicopter Society, Vol. 37, (1), January 1992, pp. 31-45.
    • (1992) Journal of the American Helicopter Society , vol.37 , Issue.1 , pp. 31-45
    • Settle, T.B.1    Kidd, D.L.2
  • 12
    • 0015331350 scopus 로고
    • Linear flap-lag dynamics of hingeless helicopter rotor blades in hover
    • April
    • Ormiston, R. A., and Hodges, D. H., "Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover," Journal of the American Helicopter Society, Vol. 17, (2), April 1972, pp. 2-14.
    • (1972) Journal of the American Helicopter Society , vol.17 , Issue.2 , pp. 2-14
    • Ormiston, R.A.1    Hodges, D.H.2
  • 13
    • 0032119906 scopus 로고    scopus 로고
    • Optimized aeroelastic couplings for alleviation of helicopter ground resonance
    • July-August
    • Gandhi, F., and Hathaway, E., "Optimized Aeroelastic Couplings for Alleviation of Helicopter Ground Resonance," Journal of Aircraft, Vol. 35, (4), July-August 1998, pp. 582-590.
    • (1998) Journal of Aircraft , vol.35 , Issue.4 , pp. 582-590
    • Gandhi, F.1    Hathaway, E.2
  • 14
    • 0004245018 scopus 로고
    • Dover Publications, New York
    • Johnson, W., Helicopter Theory, Dover Publications, New York, 1994, pp. 408-411.
    • (1994) Helicopter Theory , pp. 408-411
    • Johnson, W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.