Investigation of the Aerodynamic and Icing Characteristics of a Recessed Fuel Cell Vent Assembly III : NACA Flush-inlet-type Vent
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Ruggeri, Robert S↗
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Results for “Inlets”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Inlet Icing and Effectiveness of Hot-gas Bleedback for Ice Protection of Turbojet Engine
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Fleming, William A↗
The Use of Perforated Inlets for Efficient Supersonic Diffusion
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Evvard, John C↗
An Investigation of the Characteristics of Three NACA 1-series Nose Inlets at Subcritical and Supercritical Mach Numbers
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Pendley, Robert E↗
Theoretical and Experimental Analysis of Low-drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers of 3.30, 2.75, and 2.45
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Ferri, Antonio↗
An Investigation of the Low-speed Characteristics of Two Sharp-edge Supersonic Inlets Designed for Essentially External Supersonic Compression
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Dennard, John S↗
Velocity distributions on two-dimensional wing-duct inlets by conformal mapping
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Perl, W↗
A Low-speed Investigation of an Annular Transonic Air Inlet
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Nichols, Mark R↗
An Experimental Investigation of NACA Submerged Air Inlets on a 1/5-scale Model of a Fighter Airplane
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Gault, Donald E↗
Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets
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Jones, William L↗
Wind-tunnel Investigation of Wing Inlets for a Four-engine Airplane
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Bartlett, Walter A , Jr↗
An Experimental Investigation at Supersonic Speeds of Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer
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Davis, Wallace F↗
Experimental Investigation of Thrust Augmentation of Axial-flow-type 4000-pound-thrust Turbojet Engine by Water and Alcohol Injection at Compressor Inlet
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Baron, Burnett↗
Preliminary Investigation of Cone-type Diffusers Designed for Minimum Spillage at Inlet
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Luidens, Roger W↗
Preliminary estimate of performance of a turbojet engine when inlet pressure is reduced below exhaust pressure
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Wilsted, H D↗
A Comparison of Two Submerged Inlets at Subsonic and Transonic Speeds
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Mossman, Emmet A↗
A Preliminary Experimental Investigation of a Submerged Cascade Inlet
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Christiani, R Duane↗
Free-flight Performance of 16-inch-diameter Supersonic Ram-jet Units I : Four Units Designed for Combustion-chamber-inlet Mach Number of 0.12 at Free-stream Mach Number of 1.6 (units A-2, A-3, A-4, and A-5)
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Carlton, William W↗
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