Linked Data Explorerhttp://worldcat.org/entity/work/id/316548285
Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
A thin-layer Navier-Stokes code and a panel method code are used to predict the flow over a generic helicopter fuselage. The computational results are compared with pressure data at four experimental conditions. Both methods produce results that agree with the experimental pressure data. However, separation patterns and other viscous flow features from the Navier-Stokes code solution are shown that cannot be easily modeled with the panel method.
Open All Close All
http://schema.org/about
- http://id.worldcat.org/fast/954599
- http://id.worldcat.org/fast/954597
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/computational_fluid_dynamics
- http://id.loc.gov/authorities/subjects/sh85002823
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/navier_stokes_equations_de
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/navier_stokes_equation
- http://id.loc.gov/authorities/subjects/sh85090421
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/potential_theory
- http://id.loc.gov/authorities/subjects/sh85090420
- http://id.worldcat.org/fast/1035075
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/navier_stokes_equations
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/potentiel_theorie_du
- http://id.loc.gov/authorities/subjects/sh85060008
- http://id.worldcat.org/fast/803220
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/helicopteres_aerodynamique_modeles_mathematiques
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/fuselages
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/ecoulement_de_base_aerodynamique_simulation_par_ordinateur
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/panel_method_fluid_dynamics
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/helicopters
- http://id.loc.gov/authorities/subjects/sh85060007
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/helicopteres_aerodynamique_simulation_par_ordinateur
- http://experiment.worldcat.org/entity/work/data/316548285#Topic/flow_characteristics
- http://id.worldcat.org/fast/1035071
http://schema.org/description
- "A thin-layer Navier-Stokes code and a panel method code are used to predict the flow over a generic helicopter fuselage. The computational results are compared with pressure data at four experimental conditions. Both methods produce results that agree with the experimental pressure data. However, separation patterns and other viscous flow features from the Navier-Stokes code solution are shown that cannot be easily modeled with the panel method."@en
http://schema.org/name
- "Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment"
- "Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment"@en