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Volumn 2, Issue , 2007, Pages 1106-1124

Hover performance correlation for full-scale and model-scale coaxial rotors

Author keywords

[No Author keywords available]

Indexed keywords

CODES (STANDARDS); PARAMETER ESTIMATION; REYNOLDS NUMBER; VORTEX FLOW; WAKES;

EID: 34547876878     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (23)
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    • Arents, D. N., "An Assessment of the Hover Performance of the XH-59A Advancing Blade Concept Demonstration Helicopter," Report USAAMRDL-TN-25, Eustis Directorate, USAAMRDL, Fort Eustis, Virginia, May 1977.
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    • Full-Scale-Tunnel Investigation of the Static-Thrust Performance of a Coaxial Helicopter Rotor
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  • 9
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  • 12
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    • (2001)
    • Martin, P.B.1
  • 13
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    • Transient Dynamics of Helicopter Rotor Wakes using a Time-Accurate Free-Vortex Method,
    • Ph. D. Dissertation, University of Maryland, College park, Maryland
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  • 14
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    • Performance and Loads Data from a Hover Test of a Full-Scale XV-15 Rotor
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.