Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Alexey D. Budovsky"'
Autor:
I. D. Zverkov, Anatoly A. Maslov, Andrei A. Sidorenko, Boris Yu, Alexey D. Budovsky, V. V. Kozlov, B. V. Postnikov
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bbf2474c2dbb19328150d7016c6e2c0a
https://doi.org/10.2514/6.2009-888
https://doi.org/10.2514/6.2009-888
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
The paper deals with flight tests of dielectric barrier discharge control devices. Plasma activators were installed on sailplane’s wing and attempts to use them for control of flow separation in pre- and post- stall flight regimes were performed. M
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0154a4fe8e31ddbaabd9fc6546bb4383
https://doi.org/10.2514/6.2008-373
https://doi.org/10.2514/6.2008-373
Autor:
Alexey D. Budovsky, Norman Malmuth, Andrey A. Sidorenko, B. V. Postnikov, Anatoly A. Maslov, Boris Zanin
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Experimental study of separation control on the model of swept wing by means of dielectric barrier discharge plasma was carried out at subsonic flow speed. Surface pressure measurements, flow visualization and hot-wire anemometry data show that globa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e3c691442e92bb9cc3f29e139a68165
https://doi.org/10.2514/6.2008-540
https://doi.org/10.2514/6.2008-540
Autor:
Alexey D. Budovsky, Andrey A. Sidorenko, Norman Malmuth, Boris Zanin, Andrei Starikovskii, B. V. Postnikov, Joseph Silkey, Ivan Zavialov, Dmitry Roupassov, Philip Smereczniak
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.
Separation control experiments on a rectangular wing were carried out using dielectric barrier discharge plasma at subsonic speed for chord Reynolds numbers between 0.35 and 0.875·10. Surface pressure measurements and flow visualization show that gl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed0b176f7799480595d391913e5918c9
https://doi.org/10.2514/6.2007-941
https://doi.org/10.2514/6.2007-941
Autor:
V. Fomichev, Boris Zanin, Andrey A. Sidorenko, Alexey D. Budovsky, Anatoly A. Maslov, B. V. Postnikov, Norman Malmuth
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4962b067a6a1ebb6039e361a6450e0f
https://doi.org/10.2514/6.2005-400
https://doi.org/10.2514/6.2005-400