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An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2

An investigation of three transonic fuselage air inlets at Mach numbers from 0.4 to 0.94 and at a Mach number of 1.19

An Analysis of the Transonic and Supersonic Performance of Several Fixed-Geometry Air Inlets

Published Year

• 1950-1959 (3) *

Subject

• Aerodynamic load (1)
• Air ducts (1)
• Charts, diagrams, etc (1)
• Jet engines--Air intakes (1)
• Noses (Aircraft) (1)
• Wind tunnel testing (1)

Author

• Pendley, Robert E. (3) *
• Robinson, Harold L. (2)

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