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Meer over Aerofoil

ESDU International PLC

Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point: Single,Geometry Var: LE and TE Flaps,Initial Aerofoil: Combat Aircraft Section,CFD: BVGK (inviscid),Euler Code. 00023

€ 0,00

ESDU International PLC

Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point: Dual,Geometry Variation: LE and TE Flap Deflection and Camber Line Vars,Initial Aerofoil: RAE 2822,99021

€ 0,00

ESDU International PLC

Aerofoil Profile Drag for Mach Numbers Below the Drag Rise Condition. 00027

€ 0,00

ESDU International PLC

Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point: Single,Upper and Lower Surfaces Geometry and Camber Line Variations,Initial Aerofoil: NACA 0012 and RAE 2822,CFD: BVGK. 01025

€ 0,00

ESDU International PLC

Aerofoil and Wing Pitching Moment Coefficient at Zero Angle of Attack Due to Deployment of Trailing-edge Single-slotted Flaps at Low Speeds. 99004

€ 0,00

ESDU International PLC

Slope of Aerofoil Lift Curve for Subsonic Two-dimensional Flow. 97020

€ 0,00

ESDU International PLC

Aerofoil and Wing Pitching Moment Coefficient at Zero Angle of Attack Due to Deployment of Trailing-edge Plain Flaps at Low Speeds. 98017

€ 0,00

ESDU International PLC

Example of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Dual Design Point,Upper and Lower Surface Shape Geometry,Leading and Trailing Edge Flap Deflections,RAE 2822,Euler Code and BVGK. 01024

€ 0,00

ESDU International PLC

Aerofoil and Wing Pitching Moment Coefficient Increment at Zero Angle of Attack Due to Deployment of Leading-edge and Trailing-edge High-lift Devices in Combination at Low Speeds. 01013

€ 0,00

ESDU International PLC

Constrained Multivariate Optimisation Techniques for the Design of Aerofoil Sections 99019

€ 0,00

Boekdetails

Formaat: Loose-leaf
Uitgever: IHS ESDU
Imprint: ESDU International PLC
Auteur: ESDU International PLC, IHS ESDU
ISBN-13: 9781862460829
Verschijningsdatum: 2003-01-01

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Loose-leaf

Aerofoil and Wing Pitching Moment Coefficient at Zero Angle of Attack Due to Deployment of Trailing-edge Double-slotted and Triple-slotted Flaps at Low Speeds. 99014

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