Metody raschyeta nesushchikh kharakteristik komponovok fyuzelyazh-krylo
AUTHOR | Frolov Vladimir |
PUBLISHER | LAP Lambert Academic Publishing (01/26/2011) |
PRODUCT TYPE | Paperback (Paperback) |
Description
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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Product Format
Product Details
ISBN-13:
9783843309486
ISBN-10:
3843309485
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
Russian
More Product Details
Page Count:
148
Carton Quantity:
54
Product Dimensions:
6.00 x 0.34 x 9.00 inches
Weight:
0.50 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Technology & Engineering | Aeronautics & Astronautics
Descriptions, Reviews, Etc.
publisher marketing
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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