Flight Investigation of Engine Nacelles and Wing Vertical Position on the Drag of a Delta-Wing Airplane Configuration from Mach Number 0.8 to 2.0

Joseph H. Judd (Langley Aeronautical Laboratory, Langley Field, Va.)
naca-rm-l53l21
1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l53l21.pdf