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BACKGROUND Anonymous
Post your backgrounds!
>> Anonymous
/wg/------->
>> Anonymous
>>458901

/hr/ backgrounds
>> Anonymous
     File :-(, x)
>> Anonymous
>>458902

Try /r/, fgt.
>> Anonymous
/hr/ or /w/ its all the same u fucking nazi chan tards
>> Anonymous
>>459272
GTFO newfag.
>> Anonymous
     File :-(, x)
one of my backgrounds
>> Anonymous
     File :-(, x)
>>458899
>>458902
>>459272
>>460468

Samefag. Also, a cunt.

Go fuck yourself, this is /hr/ not /wg/.

With that in mind, this thread is now about fighter aircraft, but don't forget to sage your replies.
>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Bat Guano
     File :-(, x)
>>460537
US Grumman X-29 demonstrator from 1984 sporting advanced composites, variable-camber wing surfaces, a forward swept wing, thin supercritical airfoil, strakes, & fly-by-wire controls.
>> Bat Guano
     File :-(, x)
Two X-29 aircraft, featuring one of the most unusual designs in aviation history, flew at the Ames-Dryden Flight Research Facility (now the Dryden Flight Research Center, Edwards, California) from 1984 to 1992. The fighter-sized X-29 technology demonstrators explored several concepts and technologies including: the use of advanced composites in aircraft construction; variable-camber wing surfaces; a unique forward- swept wing and its thin supercritical airfoil; strakes; close-coupled canards; and a computerized fly-by-wire flight control system used to maintain control of the otherwise unstable aircraft.

Research results showed that the configuration of forward-swept wings, coupled with movable canards, gave pilots excellent control response at angles of attack of up to 45 degrees. During its flight history, the X-29 aircraft flew 422 research missions and a total of 436 missions. Sixty of the research flights were part of the X-29 follow-on "vortex control" phase. The forward-swept wing of the X-29 resulted in reverse airflow, toward the fuselage rather than away from it, as occurs on the usual aft-swept wing. Consequently, on the forward-swept wing, the ailerons remained unstalled at high angles of attack. This provided better airflow over the ailerons and prevented stalling (loss of lift) at high angles of attack. http://www.dfrc.nasa.gov/Gallery/Photo/X-29/HTML/EC89-0127-004.html
>> Anonymous
     File :-(, x)
needs more F-22 Raptor
>> Anonymous
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>>460665
>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
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>> Anonymous
FUCK OFF WITH THE PLANES THEY BOAR ME TO TEARS