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Y 3.N 21/5:11/E252
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The effect of compression ratio on knock limits of high-performance fuels in a CFR engine. : 3 - Blends of 2,3-dimethylpentane with 28-R / |
1 |
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Y 3.N 21/5:11/E253
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Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines. : 3 - Comparison of cooling characteristics of flight and test-stand engines / |
1 |
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Y 3.N 21/5:11/E254
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Cooling of a double-row radial engine by water injection to the individual cylinders / |
1 |
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Y 3.N 21/5:11/E255
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The effect of modified baffles and auxiliary-cooling ducts on the cooling of a double-row radial engine / |
1 |
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Y 3.N 21/5:11/E256
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Effect of NACA injection impeller and ducted head baffles on flight cooling performance of double-row radial engine in four-engine heavy bomber / |
1 |
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Y 3.N 21/5:11/E257
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Effect of fuel volatility and mixture temperature on the knocking characteristics of a liquid-cooled single-cylinder test engine / |
1 |
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Y 3.N 21/5:11/E258
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Tests of air valves for intermittent-jet engines at speeds of 20 and 25 cycles per second / |
1 |
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Y 3.N 21/5:11/E259
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Comparison of the knock-limited performance of triptane with 23 other purified hydrocarbons / |
1 |
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Y 3.N 21/5:11/E26
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Radial aircraft-engine bearing loads. : 1 - Crankpin-bearing loads for engines having nine cylinders per crankpin / |
1 |
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Y 3.N 21/5:11/E260
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Effect of internal coolants on the knock-limited performance of a liquid-cooled multicylinder aircraft engine with a compression ratio of 6.0 / |
1 |
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Y 3.N 21/5:11/E261
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Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines. : 1 - Determination of the cooling characteristics of the flight engine / |
1 |
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Y 3.N 21/5:11/E262
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Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines. : 2 - Flight knock data and comparison of fuel knock limits with engine cooling limits in flight / |
1 |
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Y 3.N 21/5:11/E263
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Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines. : 3 - Knock-limited performance of 33-R as compared with a triptane blend and 28-R in flight / |
1 |
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Y 3.N 21/5:11/E264
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Effect of water-alcohol injection and maximum-economy spark advance on knock-limited performance and fuel economy of a large air-cooled cylinder / |
1 |
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Y 3.N 21/5:11/E265
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Tests of an adjustable-area exhaust nozzle for jet-propulsion engines / |
1 |
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Y 3.N 21/5:11/E266
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Air-flow and performance characteristics of the engine-stage supercharger of a double-row radial aircraft engine. : 1 - Effect of operating variables / |
1 |
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Y 3.N 21/5:11/E267
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The effect of high-resistance ignition cable on the erosion of spark-plug electrodes / |
1 |
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Y 3.N 21/5:11/E268
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Effect of maximum cruise-power operation at ultra-lean mixture and increased spark advance on the mechanical condition of cylinder components / |
1 |
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Y 3.N 21/5:11/E269
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Sea-level performance tests of a 22-inch-diameter pulse-jet engine at various simulated ram pressures / |
1 |
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Y 3.N 21/5:11/E27
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Method of mounting cylinder blocks of in-line engines on CUE crankcases / |
1 |
