Izračun zmogljivosti letala z vertikalnim vzletom in pristankom : diplomska naloga visokošolskega strokovnega študija
Begović, Romana
V diplomskem delu je opisan matematični model za izračun optimalnega prehoda letala z vertikalnim vzletom in pristankom. Podane so osnovne enačbe mehanike leta helikopterja, letala in prehoda med ...njima. Matematični model upošteva tri povzročitelje vzgona: vzgon na disku pri poševnem obtekanja toka, vzgon, ki se ustvari zaradi induciranega toka okoli diska, ter vzgon na krilu. Izdelan algoritem omogoča izračun parametrov leta letala pri prehodu iz lebdenja v horizontalni let, pri tem pa se višina ohranja. Izračuni so opravljeni za eksperimentalno letalo s turbinskimi motorji XV-15 in za model dvosedežnega letala z batnimi motorji. Glede na dosegljive podatke v strokovni literaturi so rezultati sprejemljivi, vendar se da algoritem izboljšati z boljšim popisom zračnega toka, ki gre skozi rotor na krilo pri velikih vpadnih kotih.
Type of material - undergraduate thesis
; adult, serious
Publication and manufacture - Ljubljana : [R. Begović], 2011
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