Overview of Experiment Flight Conditions M=0.56.25000feet (Subsonic condition M=0.86.36000feef (Transonic condition) Nose-To-Tail (N2T) Distances

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Indicated Airspeed a Indicated on Instrument a Measurement of pressure on Aircraft(ie Load) O Used for structural operating limits Calibrated Airspeed a Pitot-Static Errors calibrated out a Used for Flight test and performance Groundspeed a Achieved speed over ground

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Formation Flight Basics Section v, division differences The tighter the formation the higher the workload Implications for system management Wingman uses significantly more fuel Formation flights account for 14 percent of all midairs

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