[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Li et al., 2016 - Google Patents

Aerodynamic performance and acoustic characteristics of bionic airfoil inspired by three-dimensional long-eared owl wing under low Reynolds number

Li et al., 2016

Document ID
7360246346167329458
Author
Li D
Liu X
Publication year
Publication venue
Turbo Expo: Power for Land, Sea, and Air

External Links

Snippet

The aerodynamic performance and noise of the blade are two important aspects which people pay much attention nowadays in the design of turbine machinery such as centrifugal fan and axial flow fan. In this paper, the three-dimensional model of the long-eared owl wing …
Continue reading at asmedigitalcollection.asme.org (other versions)

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • Y02T50/16Drag reduction by influencing airflow
    • Y02T50/166Drag reduction by influencing airflow by influencing the boundary layer
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources

Similar Documents

Publication Publication Date Title
Langtry et al. Predicting 2D airfoil and 3D wind turbine rotor performance using a transition model for general CFD codes
Huang et al. Simulation of shock wave buffet and its suppression on an OAT15A supercritical airfoil by IDDES
Kundu et al. Improvement of performance of S1210 hydrofoil with vortex generators and modified trailing edge
Yousefi et al. Determination of the critical Reynolds number for flow over symmetric NACA airfoils
Sogukpinar The effects of NACA 0012 airfoil modification on aerodynamic performance improvement and obtaining high lift coefficient and post-stall airfoil
Li et al. A comparative study on aerodynamic performance and noise characteristics of two kinds of long-eared owl wing models
Abdelghany et al. Air craft winglet design and performance: Cant angle effect
Khayatzadeh et al. Aerodynamic shape optimization of natural laminar flow (NLF) airfoils
Zhou et al. Implicit large eddy simulation of low Reynolds number transitional flow over a wing using high-order spectral difference method
He et al. Numerical simulation of gurney flaps lift-enhancement on a low reynolds number airfoil
Li et al. Aerodynamic performance and acoustic characteristics of bionic airfoil inspired by three-dimensional long-eared owl wing under low Reynolds number
Mohamed et al. Flow separation control using the cetacean species nose design
Sogukpinar et al. Calculation of optimum angle of attack to determine maximum lift to drag ratio of NACA 632-215 airfoil
Roy et al. A study of model separation flow behavior at high angles of attack aerodynamics
Yashodhar et al. CFD studies on triangular micro-vortex generators in flow control
Wu et al. Using the combined flow control accessory to the aerodynamic performance enhancement of bio-inspired seagull airfoils
Saha et al. Numerical investigation of gurney flap aerodynamics over a NACA 2412 airfoil
Huang et al. Numerical study of aerodynamic performance of airfoil with variable curvature split flap
Medida et al. Numerical investigation of 3-D dynamic stall using delayed detached eddy simulation
Vadyak et al. Navier-Stokes simulation of burst vortex flowfields for fighter aircraft at high incidence
Gao et al. Aerodynamic performance of a blunt trailing-edge airfoil affected by vortex generators and a trailing-edge wedge
Chishty et al. Transition prediction in low pressure turbine (LPT) using gamma theta model and passive control of separation
Omer et al. Aerodynamic Characteristics of Dimple Effect on Airfoil
Patel et al. Scale Adaptive Simulation of stalled NACA 0012 airfoil using high order schemes
Chen et al. Aerodynamic performance enhancement of tiltrotor aircraft wings using double-row vortex generators