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Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5

Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5

Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Published Year

• 1950-1959 (4)

Subject

• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Jet engines--Air intakes (1)
• Noses (Aircraft) (1)
• Pressure (1)

Author

• Sears, R. I. (4) *
• Merlet, C. F. (2)

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