The Effect of Entrance Mach Number and Lip Shape on the Subsonic Characteristics of a Scoop-type-air-induction System for a Supersonic Airplane
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Holzhauser, Curt A↗
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Comparison of Drag, Pressure Recovery, and Surface Pressure of a Scoop-type Inlet and an NACA Submerged Inlet at Transonic Speeds
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Frank, Joseph L↗
Preliminary Investigation of a Supersonic Scoop Inlet Derived from a Conical-spike Nose Inlet
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Wittliff, Charles E↗
Experimental Investigation of Internal Flow Characteristics of Forward Underslung Fuselage Scoops with Unswept Entrances at Mach Numbers of 1.41 to 1.96
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Boswinkle, Robert W , Jr↗
Experimental Investigation of the Effect of Forebody Bluntness on the Pressure Recovery and Drag of a Twin-scoop Inlet-body Combination at Mach Numbers of 1.4 and 1.7
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Stroud, John F↗
Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range
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Selna, James↗
Preliminary Investigation of a Rectangular Supersonic Scoop Inlet with Swept Sides Designed for Low Drag at a Mach Number of 2.7
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Comenzo, Raymond J↗
A Flight Comparison of a Submerged Inlet and a Scoop Inlet at Transonic Speeds
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Rolls, L Stewart↗
Performance of a Normal-shock Scoop Inlet with Boundary-layer Control
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Frazer, Alson C↗
Characteristics of a Canard-type Missile Configuration with an Underslung Scoop Inlet at Mach Numbers from 1.5 to 2.0
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Fradenburgh, Evan A↗
Effect of Circumferential Location on Angle of Attack Performance of Twin Half-conical Scoop-type Inlets Mounted Symmetrically on the RM-10 Body of Revolution
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Valerino, Alfred S↗
Experimental Investigation of the Effect of Entrance Width-to-height Ratio on the Performance of an Auxiliary Scoop-type Inlet at Mach Numbers from 0 to 1.3
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Brajnikoff, George B↗
Investigation at a Mach Number of 1.90 of a Diverter-type Boundary-layer Removal System for a Scoop Inlet
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Kochendorfer, Fred D↗
Investigation of Aerodynamic and Icing Characteristics of a Flush Alternate-inlet Induction-system Air Scoop
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Lewis, James P↗
The performance of conical supersonic scoop inlets on circular fuselages
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Hasel, Lowell E↗
Angle-of-attack-supersonic performance of a configuration consisting of a ramp-type scoop inlet located either on top or bottom of a body of revolution
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Kremzier, Emil J↗
Investigation of a Flow Deflector and an Auxiliary Scoop for Improving Off-design Performance of Nose Inlets
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Anderson, Warren E↗
Performance of a Supersonic Ramp Inlet with Internal Boundary-layer Scoop
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Campbell, Robert C↗