Harrier has none.
The channel loss on the Pegasus engine was some 200 lbs of thrust less when installed and pointing the nozzles at 90 degrees.
really good intake design next to no intake basically and the auxiallry air intakes help a lot
As do they boundary layer doors.
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yeah it shows you can midigate the effects of channel loss by designing properly in a plane with TVC
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Cats can squeeze into the tiniest gaps— That’s true for both the F-14 fighter jet and the animal kind
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bring back upgraded legacy hornet as an A-4/A-7 type and replace F/A-18E with F/A-XX, then use upgraded F-35C’s like F-4J’s
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You can’t have multiple planes in the same message you need to make separate messages for each one. Otherwise it won’t count.
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this for F-14A early.
and this for F-14B
Thank you now im make it sperarated.
f-15 same br as the f-14a r we deadass vro
I make that suggess now.
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Tbh I don’t think we need compression as more of we need decompression also giving the F-14A aim7m with aim9L and F-14B aim7mh or aim7P with aim9m
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