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Dimensionamento di un turbopropulsore

Study material for Propulsione Aerospaziale, shared by the Studwiz community and reviewed by moderators.

Propulsione AerospazialeComplete set

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p,eq c 1500 a a qf p ⌘p,el=0.85 ⌘d ⌘c ⌘mc ⌘b ⌘pb ⌘t ⌘mt ⌘r ⌘u hu ˙ma ˙mel p,eq p,el p,j u9' p 2( 1 ) hu⌘u Pp,j=˙maV(u9 V) Pp,el=˙ma⌘p,el⌘t⌘m,t⌘r hu @Pp @ =0 opt=1 ⌘uV2 2(⌘r⌘t⌘mt⌘p,el)2(1 +f) hu f=˙mfu e l ˙ma • • • T0a=T2=T0 ✓ 1+k 1 2M2 ◆ ⌘d 8 >>>< >>>: ⌘d=T20 Ta T2 Ta p0 2=p2=p02=pa ✓T20 Ta ◆k k 1 c 2 3 ⌘c 3 T3>T30 8 < : p3=p2 c ⌘c=T30 T2 T3 T2 ⌘b ⌘pb f hf= cp,fTf qf f ( p4=p3⌘pb (˙ma+˙mf)h4=˙mah3+˙mfhf+˙mfqf⌘b Lt Lc ⌘mtLt=Lc ⌘mc ⌘t

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First page: Dimensionamento di un turbopropulsore