PPT Slide
Compact Inlets Lead to Lower
Aircraft Empty Weight
Inlet Volume Fraction
(Inlet Duct Volume / Aircraft Volume)
Inlet Weight Fraction
(Inlet Weight / Aircraft Empty Weight)
0.00
0.01
0.02
0.03
0.04
0.05
0.06
0.06
0.07
0.08
0.09
0.10
0.11
0.12
F-16
F-22
F-14
F/A-18
F-15
No Moving Parts
Multiple Moving Parts
F-111
Technology Prioritization: Selected Technology Set
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