Author: Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Optimization of an Advanced Design Three-element Airfoil at High Reynolds Numbers ... Nasa-tm-112019 ... Nasa
Author: Optimization of an Advanced Design Three-element Airfoil at High Reynolds Numbers
Author: J. C. LinHigh Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author: William Garland JohnsonPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 176
Book Description
Multi-element Airfoil Optimization for Maximum Lift at High Reynolds Numbers
Author: Walter O. ValarezoProfile Optimization Method for Robust Airfoil Shape Optimization in Viscous Flow
Author: Wu LiProfile Optimization Method for Robust Airfoil Shape Optimization in Viscous Flow
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781721572281
Category :
Languages : en
Pages : 28
Book Description
Simulation results obtained by using FUN2D for robust airfoil shape optimization in transonic viscous flow are included to show the potential of the profile optimization method for generating fairly smooth optimal airfoils with no off-design performance degradation. Li, Wu Langley Research Center NASA/TM-2003-212408, L-18283, NAS 1.15:212408
Aerodynamic Performance and Pressure Distributions for a NASA SC(2)-0714 Airfoil Tested in the Langley 0.3-meter Transonic Cryogenic Tunnel
Author: Renaldo V. JenkinsPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 308
Book Description
Airfoil Design by Numerical Optimization Using a Minicomputer
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781724230096
Category :
Languages : en
Pages : 28
Book Description
A computer program developed for the automated design of low speed airfoils utilizes a generalized Joukowski method for aerodynamic analysis coupled with a conjugate gradient, penalty function, numerical optimization algorithm to give an efficient calculation technique for use with minicomputers. The program designs airfoils with a prescribed pressure distribution as well as those which minimize or maximize some aerodynamic force coefficient. At present the method is restricted to inviscid, incompressible flow. A typical design problem will execute in 4.5 hr on an HP 9830 minicomputer. Hicks, R. M. and Szelazek, C. A. Ames Research Center NASA-TM-78502, A-7505 RTOP 505-10-11-01
Pressure Distributions from High Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author: William Garland JohnsonPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 416
Book Description
Aerodynamic Performance and Pressure Distributions for a NASA SC(2)-0714 Airfoil Tested in the Langley 0.3-meter Transonic Cryogenic Tunnel
Author: Renaldo V. JenkinsPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 308
Book Description