Preliminary Experiments with Pilot Burners for Ram-jet Combustors
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Farley, John M↗
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Performance Comparison of Three Canard-type Ram-jet Missile Configurations at Mach Numbers from 1.5 to 2.0
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Fradenburgh, Evan A↗
Effect of fuel injector location and mixture control on performance of a 16-inch ram-jet can-type combustor
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Cervenka, A J↗
Transonic Free-flight Investigation of the Total Drag and of the Component Drags (cowl Pressure, Additive, Base, Friction, and Internal) Encountered by a 16-inch-diameter Ram-jet Engine for Mach Numbers from 0.80 to 1.43
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Messing, Wesley E↗
Magnesium-slurry Combustion Performance in 6.5-inch-diameter Ram-jet Engine Mounted in Connected-pipe Facility
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Branstetter, J Robert↗
Free-jet Investigation of a 20-inch Ram-jet Combustor Utilizing High-heat-release Pilot Burner
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Henzel, James G , Jr↗
Evaluation of End- and Radial-burning Solid Fuels in Ram Jets Mounted in a Free Jet at Mach Numbers of 2.0, 2.2, and 2.3
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Bartlett, Walter A , Jr↗
A Theory for Stability and Buzz Pulsation Amplitude in Ram Jets and an Experimental Investigation Including Scale Effects
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Trimpi, Robert L↗
Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
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Radin, Edward J↗
Effect of fuels on combustion efficiency of 5-inch ram-jet-type combustor
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Reynolds, Thaine W↗
Investigation at Mach Numbers 2.98 and 2.18 of Axially Symmetric Free-jet Diffusion with a Ram-jet Engine
An investigation was conducted to determine the effectiveness of a free-jet diffuser in reducing the over-all pressure ratios required to operate a free jet with a large air-breathing engine as a test vehicle. Efficient operation of the free jet was determined with and without the considerations required for producing suitable engine-inlet flow conditions. A minimum operating pressure ration of 5.5 was attained with a ratio of nozzle-exit to engine-inlet area of 1.85. Operation of the free jet with unstable engine-inlet flow (buzz) is also included.
WIND TUNNELS↗
Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges : Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.60
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Spearman, M Leroy↗
Preflight Tests and Flight Performance of a 6.5-inch Diameter Ram-jet Engine
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Hinners, Arthur H , Jr↗
Flight and Preflight Evaluation of an Automatic Thrust-coefficient Control System in a Twin-engine Ram-jet Missile
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Dettwyler, H Rudolph↗
Effect of inlet-air temperature on performance of a 16-inch ram-jet combustor
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Cervenka, A J↗
Initial performance investigation of pentaborane fuel in free-flight ram-jet engine
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Disher, John H↗
Flight Investigation to Determine Lift and Drag Characteristics of a Canard Ram-jet Missile Configuration in the Mach Number Range of 0.8 to 2.0
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Gammal, Abraham A↗
Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.5 to 2.16
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Hearth, Donald P↗