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Numerical Study Of The Trailing Vortex Of A Wing With Wing Tip Blowing
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Book Synopsis Numerical Study of the Trailing Vortex of a Wing with Wing-tip Blowing by : Hock-Bin Lim
Download or read book Numerical Study of the Trailing Vortex of a Wing with Wing-tip Blowing written by Hock-Bin Lim and published by . This book was released on 1994 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723239106 Total Pages :160 pages Book Rating :4.2/5 (391 download)
Book Synopsis Numerical Study of the Trailing Vortex of a Wing with Wing-Tip Blowing by : National Aeronautics and Space Administration (NASA)
Download or read book Numerical Study of the Trailing Vortex of a Wing with Wing-Tip Blowing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-18 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt: Trailing vortices generated by lifting surfaces such as helicopter rotor blades, ship propellers, fixed wings, and canard control surfaces are known to be the source of noise, vibration, cavitation, degradation of performance, and other hazardous problems. Controlling these vortices is, therefore, of practical interest. The formation and behavior of the trailing vortices are studied in the present research. In addition, wing-tip blowing concepts employing axial blowing and spanwise blowing are studied to determine their effectiveness in controlling these vortices and their effects on the performance of the wing. The 3D, unsteady, thin-layer compressible Navier-Stokes equations are solved using a time-accurate, implicit, finite difference scheme that employs LU-ADI factorization. The wing-tip blowing is simulated using the actuator plane concept, thereby, not requiring resolution of the jet slot geometry. Furthermore, the solution blanking feature of the chimera scheme is used to simplify the parametric study procedure for the wing-tip blowing. Computed results are shown to compare favorably with experimental measurements. It is found that axial wing-tip blowing, although delaying the rolling-up of the trailing vortices and the near-field behavior of the flowfield, does not dissipate the circulation strength of the trailing vortex farther downstream. Spanwise wing-tip blowing has the effect of displacing the trailing vortices outboard and upward. The increased 'wing-span' due to the spanwise wing-tip blowing has the effect of lift augmentation on the wing and the strengthening of the trailing vortices. Secondary trailing vortices are created at high spanwise wing-tip blowing intensities. Lim, Hock-Bin Unspecified Center BLOWING; COMPUTERIZED SIMULATION; CONTROL SURFACES; FINITE DIFFERENCE THEORY; LIFT AUGMENTATION; NAVIER-STOKES EQUATION; ROTARY WINGS; ROTOR BLADES; SPANWISE BLOWING; VORTICES; WINGS; CANARD CONFIGURATIONS; CAVITATION FLOW; DIFFERENCE EQUATIONS; DISSI...
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis Low-Speed Aerodynamics by : Joseph Katz
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