Author: Cuyler W. Brooks
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil: Suction Coefficient Analysis
The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil
The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil
Author: Cuyler W. Brooks
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 48
Book Description
The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil - Drag Equations
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722873516
Category :
Languages : en
Pages : 42
Book Description
The Langley Research Center has designed a swept, supercritical airfoil incorporating Laminar Flow Control for testing at transonic speeds. Analytical expressions have been developed and an evaluation made of the experimental section drag, composed of suction drag and wake drag, using theoretical design information and experimental data. The analysis shows that, although the sweep-induced boundary-layer crossflow influence on the wake drag is too large to be ignored and there is not a practical method for evaluating these crossflow effects on the experimental wake data, the conventional unswept 2-D wake-drag computation used in the reduction of the experimental data is at worst 10 percent too high. Brooks, Cuyler W., Jr. and Harris, Charles D. and Harvey, William D. Langley Research Center RTOP 505-60-31-03...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722873516
Category :
Languages : en
Pages : 42
Book Description
The Langley Research Center has designed a swept, supercritical airfoil incorporating Laminar Flow Control for testing at transonic speeds. Analytical expressions have been developed and an evaluation made of the experimental section drag, composed of suction drag and wake drag, using theoretical design information and experimental data. The analysis shows that, although the sweep-induced boundary-layer crossflow influence on the wake drag is too large to be ignored and there is not a practical method for evaluating these crossflow effects on the experimental wake data, the conventional unswept 2-D wake-drag computation used in the reduction of the experimental data is at worst 10 percent too high. Brooks, Cuyler W., Jr. and Harris, Charles D. and Harvey, William D. Langley Research Center RTOP 505-60-31-03...
The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil
Author: Cuyler W. Brooks (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 28
Book Description
The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil
Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 132
Book Description