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F-16AT "Falcon 21"


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energo
PostPosted: May 15, 2011 - 06:19 PM Reply with quote Back to top
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"Supersonic Aerodynamic Characteristics of an
Advanced F-16 Derivative Aircraft Configuration"

NASA Technical Paper 3355

Source: LINK1 LINK2

Quote:
Summary
An investigation has been made at Mach num-
bers of 1.60 to 2.16 to determine the longitudinal and
lateral-directional characteristics of an advanced air-
craft con guration. The aircraft concept is a deriva-
tive of the United States Air Force F-16C multirole
fighter...


Enjoy!

B. Bolsøy
Oslo


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NASA Technical Paper 3355 - Supersonic Aerodynamic Characteristics of an
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Falcon2110.1.1.51.2771.pdf
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NASA Technical Paper 3355 - Supersonic Aerodynamic Characteristics of an
Advanced F-16 Derivative Aircraft Configuration

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