Passage: Located behind the leading edge of the wing the engine intake had wing boundary layer ahead of it. Two thirds was diverted and the remaining third which entered the intake did not adversely affect the intake efficiency except during pushovers when the boundary layer thickened ahead of the intake and caused surging. Extensive wind tunnel testing helped define leading edge modifications ahead of the intakes which solved the problem.Each engine had its own intake and the engine nacelles were paired with a splitter plate between them to minimize adverse behavior of one powerplant influencing the other. Mach 1.6 only above was an engine surge likely to affect the adjacent engine. Mach 1.6 nikan loke ni okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okunfa okun
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