Tests of Several Model Nacelle-propeller Arrangements in Front of a Wing
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INTERFERENCE-WINGS & NACELLE-PROPELLER COMBINATION↗
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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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Drag and Propulsive Characteristics of Air-cooled Engine-nacelle Installations for Two-engine Airplanes
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PROPELLERS-PROPULSIVE EFFICIENCY↗
Some Lift and Drag Measurements of a Representative Bomber Nacelle on a Low-drag Wing I
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LIFT & DRAG↗
Some Lift and Drag Measurements of a Representative Bomber Nacelle on a Low-drag Wing II
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INTERFERENCE - NACELLE & WINGS↗
Effects of a typical nacelle on the characteristics of a thick low-drag airfoil critically affected by leading-edge roughness
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ENGINE NACELLES↗
Some Lift and Drag Measurements of Two Configurations of a Nacelle and Oil-cooler Scoop for the Hughes-kaiser Cargo Airplane
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WIND TUNNEL TESTS (NACA - PRESSURE, LOW-TURBULENCE↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGE-STORE CONFIGURATIONS. II - SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE. LATERAL FORCES AND PITCHING MOMENTS, MACH NUMBER, 1.61
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moments
SWEPT WING↗
Investigation of the Effects of a Nacelle on the Aerodynamic Characteristics of a Swept Wing and the Effects of Sweep on a Wing Alone
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WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')↗
Vibratory Stresses in Propellers Operating in the Flow Field of a Wing-nacelle-fuselage Combination
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LOADS - PROPELLERS↗
The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel with and Without Nacelles at Mach Numbers from 0.30 to 0.86
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WING - NACELLE COMBINATIONS - AIRPLANES↗
A Comparison at High Speed of the Aerodynamic Merits of Models of Medium Bombers Having Thickened Wing Roots and Having Wings with Nacelles
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ENGINES- INSTALLATION↗
Ground-stand Cooling Investigation of an R-2600-22 Engine in a PBM-3D Nacelle
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ENGINES-WRIGHT R-2600-22 (AMER )↗
Cooling investigation of a B-24D engine-nacelle installation in the NACA full-scale tunnel
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SUPERCHARGERS, TURBO↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. 1.-SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE . LIFT AND DRAG, MACH NUMBER, 1.61
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
EXTERNAL STORE↗
THE ORIGIN AND DISTRIBUTION OF SUPSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. V - SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE. MACH NUMBER 2.01
Origin & distribution of supersonic store interference/measurement of individual forces - swept-wing heavy bomber with large store figure
EXTERNAL STORE↗
Preliminary transonic performance results for solid and slotted turbojet nacelle afterbodies incorporating fixed divergent jet nozzles designed for supersonic operation
Transonic performance of three turbojet nozzle- afterbody configurations
JET NOZZLE↗
Prediction of first-order vibratory stresses for a propeller operating in the flow field of a wing-nacelle-fuselage combination
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Rogallo, V. L.↗
Experimental investigation of a new type of low-drag wing-nacelle combination
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Allen, H. J.↗