Estudio del comportamiento aerodinámico de los perfiles Naca 4415 y Naca 64514 durante los despegues, aterrizajes y vuelos a bajas alturas. Aplicación del software Fluent v6.3.26
Main Author: | Meza torres,Rubén Darío |
---|---|
Format: | Others |
Language: | es |
Published: |
Universidad Nacional de Ingeniería. Programa Cybertesis PERÚ
2008
|
Online Access: | http://cybertesis.uni.edu.pe/uni/2008/meza_tr/html/index-frames.html |
Similar Items
-
Computational study of a NACA4415 airfoil using synthetic jet control
by: Lopez Mejia, Omar Dario
Published: (2011) -
CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge.
by: S M A Aftab, et al.
Published: (2017-01-01) -
Prediction of Aerodynamics Coefficients of Modified NACA 4415 Airfoil Using Computational Fluid Dynamics
by: Sudarsono, et al.
Published: (2020-01-01) -
Correction: CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge.
by: S M A Aftab, et al.
Published: (2017-01-01) -
SIMULATION OF LOW-RE FLOW OVER A MODIFIED NACA 4415 AIRFOIL WITH OSCILLATING CAMBER
by: Katam, Vamsidhar
Published: (2005)