Call Number (LC) Title Results
Y 3.N 21/5:11/E23 Thermodynamic data for the computation of the performance of exhaust-gas turbines / 1
Y 3.N 21/5:11/E230 The knock-limited performance of fuel blends containing aromatics. : 3-1,3,5-trimethylbenzene, tert-butylbenzene, and 1,2,4-trimethylbenzene / 1
Y 3.N 21/5:11/E231 The knock-limited performance of fuel blends containing aromatics. : 4 - Data for m-diethylbenzene, 1-ethyl-4-methylbenzene and sec-butylbenzene together with a summarization of data for 12 aromatic hydrocarbons / 1
Y 3.N 21/5:11/E232 The effect of inlet temperature and pressure on the efficiency of a single-stage impulse turbine having a 13.2-inch pitch-line diameter wheel / 1
Y 3.N 21/5:11/E233 The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades / 1
Y 3.N 21/5:11/E234 Calculations of the performance of a compression-ignition engine-compressor turbine combination. : 1 - Performance of a highly supercharged compression-ignition engine / 1
Y 3.N 21/5:11/E235 Knock-limited performance of pure hydrocarbons blended with a base fuel in a full-scale, aircraft-engine cylinder. : 3 - Four aromatics, six ethers / 1
Y 3.N 21/5:11/E236 Knock-limited performance tests of 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene in small-scale and full-scale cylinders / 1
Y 3.N 21/5:11/E237 The knock-limited performance of fuel blends containing aromatics. : 5 - n-propylbenzene, n-butylbenzene, isobutylbenzene, m-xylene, and 1-isopropyl-4-methylbenzene / 1
Y 3.N 21/5:11/E238 Relation between spark-ignition engine knock, detonation waves, and autoignition as shown by high-speed photography / 1
Y 3.N 21/5:11/E239 Analysis of spark-ignition engine knock as seen in photographs taken at 200,000 frames a second / 1
Y 3.N 21/5:11/E24 Some effects of internal coolants on knock-limited and temperature-limited power as determined in a single-cylinder aircraft test engine / 1
Y 3.N 21/5:11/E240 A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine - 2 / 1
Y 3.N 21/5:11/E241 Performance charts for a turbojet system / 1
Y 3.N 21/5:11/E242 Knock-limited blending characteristics of blends of triptane and 28-R aviation fuel / 1
Y 3.N 21/5:11/E243 A preliminary evaluation of the explosion jet-propulsion engine / 1
Y 3.N 21/5:11/E244 Effect of water injection on knock-limited performance of a V-type 12-cylinder liquid-cooled engine / 1
Y 3.N 21/5:11/E245 The effect of compression ratio on knock limits of high-performance fuels in a CFR engine. : 1 - Blends of triptane and 28-R fuel / 1
Y 3.N 21/5:11/E246 F-3 and F-4 engine tests of several high-antiknock components of aviation fuel / 1
Y 3.N 21/5:11/E247 Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines. : 1 - Determination of cooling characteristics of flight engine / 1