Plasma Control of Vortex Flow on Delta-Wing at High Angles of Attack

Autor: I. D. Zverkov, Anatoly A. Maslov, Andrei A. Sidorenko, Boris Yu, Alexey D. Budovsky, V. V. Kozlov, B. V. Postnikov
Rok vydání: 2009
Předmět:
Zdroj: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
DOI: 10.2514/6.2009-888
Popis: Nomenclature AR = wing aspect ratio b = wing thickness Cp = pressure coefficient, (p-p0)/q+1 c = wing root chord length Cxa = drag coefficient Cya = lift coefficient Cza = side force coefficient K = lift-drag ratio, mxa = roll moment coefficient mza = pitching moment coefficients p = static pressure on the model surface Tu = free-stream turbulence level, % of U∞ U∞ = mean free-stream velocity q = dynamic pressure x = vortex breakdown position along the wing chord z = transversal direction along the wing span α = angle of attack χ = delta-wing leading edge sweep angle
Databáze: OpenAIRE