Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
Fuel Value (liters)<br />
AHS Forum 58, June 2002<br />
Fuel Value<br />
W = W + W + W + W<br />
0<br />
3000<br />
2500<br />
2000<br />
1500<br />
1000<br />
500<br />
0<br />
����� PL �����<br />
F �C<br />
E<br />
W<br />
U<br />
Database configurations<br />
Estimation<br />
0 500 1000 1500 2000 2500 3000<br />
Fuel Values Estimation (liters)<br />
W<br />
F<br />
Rg<br />
0 0038 W 0976 Rg 0650,<br />
0<br />
= Range with standard fuel at sea level<br />
( AVER = 11%, MAX = 33%, R = .9942),<br />
where WFis fuel value in [ liters], W0is<br />
in [ kg]<br />
,<br />
and is range with standard fuel, S/ L in [ km]<br />
.<br />
Rg<br />
ε ε<br />
= . . .<br />
<strong>Faculty</strong> <strong>of</strong> <strong>Aerospace</strong> Eng., Technion - I.I.T.<br />
29
Change language