Overview

"Kniga yavlyaetsya dissertatsiey na soiskanie uchyenoy stepeni kandidata tekhnicheskikh nauk, v kotoroy rassmatrivayutsya voprosy teoreticheskoy otsenki pod""yemnoy sily razlichnykh po geometrii komponovok fyuzelyazh-krylo letatel'nykh apparatov. Metody, predstavlennye v knige, otnosyatsya k priblizhyennym ili inzhenernym metodam, ne trebuyushchim bol'shikh komp'yuternykh resursov. V ramkakh teorii polos polucheny analiticheskie formuly dlya koeffitsientov interferentsii. Predstavleny chislennye modeli raschyeta aerodinamicheskikh kharakteristik komponovok fyuzelyazha i kryla s ispol'zovaniem metoda diskretnykh vikhrey dlya nesushchey poverkhnosti i razlichnykh modeley potentsial'nykh techeniy okolo 2D poperechnykh secheniy fyuzelyazha (analiticheskiy, chislenno-analiticheskiy i panel'nyy metody). Kniga soderzhit analiticheskiy obzor po probleme interferentsii v sisteme ""fyuzelyazh-krylo"" i glavu po optimizatsii. Dostovernost' predlozhennykh metodov podtverzhdaetsya mnogochislennymi sravneniyami rezul'tatov raschyetov s teoreticheskimi i eksperimental'nymi dannymi drugikh issledovateley i samogo avtora. Kniga prednaznachena dlya prepodavateley i nauchnykh sotrudnikov universitetov, inzhenerov i studentov, izuchayushchikh aerodinamiku letatel'nykh apparatov."

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