'Tip vortex' diaporamas de présentation

Prediction of Rotorcraft Noise with A Low-Dispersion Finite Volume Scheme

A Thesis Proposal Presented to The Faculty of the Division of Graduate Studies By Gang Wang Advisor: Dr. T. C. Lieuwen. Prediction of Rotorcraft Noise with A Low-Dispersion Finite Volume Scheme. Background Approach Results Conclusions Proposed Work. OUTLINE.

595 views • 47 slides

Uncontrolled copy not subject to amendment

Uncontrolled copy not subject to amendment. Principles of Flight. Principles of Flight. Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane in flight Part 2. Principles of Flight. Revision. Questions.

534 views • 40 slides

Uncontrolled copy not subject to amendment

Uncontrolled copy not subject to amendment. Principles of Flight. Principles of Flight. Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane in flight Part 2. Principles of Flight. Revision. Questions.

691 views • 40 slides

Uncontrolled copy not subject to amendment

Uncontrolled copy not subject to amendment. Principles of Flight. Principles of Flight. Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane in flight Part 2. Principles of Flight. Revision. Questions.

408 views • 40 slides

High Order DNS and LES for Wing Tip Vortex and Flow Control Hua Shan, Li Jiang, Chaoqun Liu

High Order DNS and LES for Wing Tip Vortex and Flow Control Hua Shan, Li Jiang, Chaoqun Liu Department of Mathematics University of Texas at Arlington Arlington, TX 76019 (Supported by ONR, AFOSR, Lockheed, AFRL). February 2008. Outline. 1. Introduction.

581 views • 37 slides

High Order DNS and LES for Wing Tip Vortex and Flow Control Hua Shan, Li Jiang, Chaoqun Liu

High Order DNS and LES for Wing Tip Vortex and Flow Control Hua Shan, Li Jiang, Chaoqun Liu Department of Mathematics University of Texas at Arlington Arlington, TX 76019 (Supported by ONR, AFOSR, Lockheed, AFRL). February 2008. Outline. 1. Introduction.

376 views • 37 slides

Numerical and Experimental Analysis of Performance and Aerodynamic Loads on HAWT Blade

Numerical and Experimental Analysis of Performance and Aerodynamic Loads on HAWT Blade. AeroAcoustics & Noise Control Laboratory, Seoul National University Jiwoong Park, Hyungki Shin, Hogeon Kim, Soogab Lee. Introduction. Numerical Method. Experimental Method. Results & Analysis.

441 views • 29 slides

RANS predictions of a cavitating tip vortex

228 views • 12 slides