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Wind-tunnel investigation at Mach numbers from 0.25 to 1.01 of a transport configuration designed to cruise at near-sonic speeds. [conducted in langley 8-foot transonic pressure tunnel]

R. A. Langhans, S. G. Flechner

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Key concepts: Transonic, Cruise, Mach number, Subsonic and transonic wind tunnel, Wind tunnel, Sonic boom, Supersonic wind tunnel, Hypersonic wind tunnel

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Wind-tunnel investigation at Mach numbers from 0.25 to 1.01 of a transport configuration designed to cruise at near-sonic speeds. [conducted in langley 8-foot transonic pressure tunnel] — Research Paper | ScholarLens