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Euler calculations for flowfield of a helicopter rotor in hover
R. K. Agarwal
, J. E. Deese
Department of Mechanical Engineering & Materials Science
Roy and Diana Vagelos Division of Biology & Biomedical Sciences (DBBS)
Research output
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Contribution to journal
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Article
›
peer-review
63
Scopus citations
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Keyphrases
Flow Field
100%
Absolute Flow
100%
Leonhard Euler
100%
Helicopter Rotor
100%
Rotor in Hover
100%
Flow Variables
66%
Euler Equations
66%
Analysis Program
33%
Finite Volume
33%
Angle of Attack
33%
Jameson
33%
Explicit Runge-Kutta
33%
Curvilinear Grids
33%
Time-stepping Scheme
33%
Pitch Angle
33%
Aerodynamic Loads
33%
Hovering Flight
33%
Wake Effect
33%
Relative Flow
33%
Rotor Wake
33%
Downwash
33%
Rotating Coordinate System
33%
Wake Analysis
33%
Geometric Angle
33%
Free Wake
33%
Collective pitch
33%
Model Helicopter
33%
Engineering
Helicopter Rotors
100%
Euler Equation
66%
Flow Variable
66%
Rotors
33%
Angle-of-Attack
33%
Downwash
33%
Stepping Scheme
33%
Pitch Angle
33%
Aerodynamic Load
33%
Rotating Coordinate System
33%