Aeroelastic of transient blade dynamics during shipboard engage/disengage operations

Journal of Aircraft

Volumn 35, Issue 3, 1998, Pages 445-453

  Geyer Jr , William P ^a,c,d   Smith, Edward C ^b,d,e   Keller, Jonathan A ^b,d,e  

^a US Naval Air Warfare Center   (United States)

^b PENNSYLVANIA STATE UNIVERSITY   (United States)

^c Naval AirWarfare Center   (United States)

^d AIAA   (United States)

^e Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; EQUATIONS OF MOTION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; TORSIONAL STRESS; UNSTEADY FLOW; WIND EFFECTS;

HAMILTON'S PRINCIPLE; SHIPBOARD ENGAGE/DISENGAGE SEQUENCES; TRANSIENT BLADE DYNAMICS;

HELICOPTER ROTORS;

EID: 0032072544     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2317     Document Type: Article

References (15)

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