IN2012DE00300A - - Google Patents

Info

Publication number
IN2012DE00300A
IN2012DE00300A IN300DE2012A IN2012DE00300A IN 2012DE00300 A IN2012DE00300 A IN 2012DE00300A IN 300DE2012 A IN300DE2012 A IN 300DE2012A IN 2012DE00300 A IN2012DE00300 A IN 2012DE00300A
Authority
IN
India
Prior art keywords
air
lift
vortices
low reynolds
applications
Prior art date
Application number
Other languages
English (en)
Inventor
Gargeshwari Krishnamurthy Suryanarayana
Vidyadhar Yogeshwar Mudkavi
Original Assignee
Council Scient Ind Res
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Council Scient Ind Res filed Critical Council Scient Ind Res
Priority to IN300DE2012 priority Critical patent/IN2012DE00300A/en
Publication of IN2012DE00300A publication Critical patent/IN2012DE00300A/en

Links

IN300DE2012 2012-02-03 2012-02-03 IN2012DE00300A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IN300DE2012 IN2012DE00300A (zh) 2012-02-03 2012-02-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IN300DE2012 IN2012DE00300A (zh) 2012-02-03 2012-02-03

Publications (1)

Publication Number Publication Date
IN2012DE00300A true IN2012DE00300A (zh) 2015-04-10

Family

ID=54393640

Family Applications (1)

Application Number Title Priority Date Filing Date
IN300DE2012 IN2012DE00300A (zh) 2012-02-03 2012-02-03

Country Status (1)

Country Link
IN (1) IN2012DE00300A (zh)

Similar Documents

Publication Publication Date Title
Patel et al. CFD Analysis of an Aerofoil
WO2013106120A3 (en) Device, assembly, and system for reducing aerodynamic drag
US20160280358A1 (en) Hybrid Flow Control Method for Simple Hinged Flap High-Lift System
Wang et al. Stall control with feathers: Self-activated flaps on finite wings at low Reynolds numbers
WO2011041991A3 (en) Aircraft using ducted fan for lift
EP2327628A3 (en) Methods and systems for minimizing flow disturbances in aircraft propeller blades caused by upstream pylons
Genç et al. Effect of tip vortices on flow over NACA4412 aerofoil with different aspect ratios
IN2012DE00300A (zh)
Marques Emerging technologies in UAV aerodynamics
RU2008152296A (ru) Способ и устройство для создания аэродинамического сопротивления на самолете
Crivoi et al. Some experimental results on Coanda effect with application to a flying vehicle
Lee et al. Actuations of synthetic jets on a UCAV planform at high angles of attack
Asada Computational analysis of the flow fields induced by a DBD plasma actuator toward separated-flow control
Jafarzade et al. Influence of wingtips on induced drag force of rectangular wing."
WO2013107946A3 (fr) Aeronef
RU2534489C1 (ru) Носовая часть летательного аппарата (варианты)
Sznajder et al. Analysis of effects of shape and location of micro-turbulators on unsteady shockwave-boundary layer interactions in transonic flow
Qiao et al. The investigation of the airfoil for the small wind turbine based on the seagull airfoil
Bechert et al. Self-actuating flaps on bird and aircraft wings
Saiteja et al. Computational analysis of slotted wing tips at low Reynolds number
Naderi et al. Experimental investigation of grid winglet effects on aerodynamic characteristics of a wing model at low Reynolds number
Cho et al. Control of wing-tip vortex using winglets at low Reynolds number
SK Numerical Analysis of Flow Over Fixed Wing Mav with Bio Inspired Winglets
Udartsev et al. Improvement of UAV navigation reliability at high angles of attack
Yang Investigations of super-lifting co-flow jet airfoil and distributed electric propulsion aircraft