Vortex as a means of improving educational aerodynamic characteristics of aircraft
DOI:
https://doi.org/10.18372/2306-1472.31.1450Abstract
Examine matter using the Vortex Generator like instrument for lead in hair angel of attack or for prevention tearing off turbulent flow boundary layer from component airplane without energy consumption.
References
Udartsev E. P. Dr Sci (eng). Problems of airplane unsteady aerodynamics // Proceeding of the national aviation university. – 2005. – № 2. – Р. 41–44.
Чжен П. Управление отрывом потока. – М: Мир, 1979. – 552 с.
Flow structure in the wake of a wishbone vortex generator. Wendt.b.j., Hingst W.R // AIAA journal. – 1994. – 32, № 11. – Р. 2234–2240.
KNOW-BLADE Task-2 report; Aerodynamic Accessories. Jeppe Johansen, Niels N., Sørensen Risø National Laboratory Rockslide Denmark. – October. – 2004.
Know-blade Task-3.3 report; Rotor Blade Computations with 3D Vortex Generators Jeppe Johansen, Niels N. Sørensen, Risø National Laboratory Rockslide Denmark. – January. – 2005.
Michael F. Kerho and Brian R. Kramer (Enhanced Airfoil Design Incorporating Boundary Layer Mixing Devices) 41st AIAA Aerospace Sciences Meeting & Exhibit 6-9 January 2003 / Reno, NV.
Michatl kerho and brian kramer (enhanced airfoil design incorporating boundary layer mixing Devices) AIAA-2003-0211.
Chima, Rodrick V.: Calculation of Multistage Turbomachinery Flow Using Steady Characteristic Boundary Conditions. AIAA Paper 98-0968. – Jan. – 1998. (NASA/TM-1998-206613).
Ola Logdberg ( vortex generators and turbulent boundary layer separation control ) October 2006 Technical Reports from Royal Institute of Technology KTH Me-chanics SE-100 44. – Stockholm, Sweden.