5,319 research outputs found

    Experimental evaluation of a TF30-P-3 turbofan engine in an altitude facility: Effect of steady-state temperature distortion

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    The effects of circumferential distortion of the total temperature entering 25, 50, and 75 percent of the inlet circumferential annulus of a turbofan engine were determined. Complete compressor stall resulted from distortions of from 14 to 20 percent of the face averaged temperature. Increasing the temperature level in one sector resulted in that sector moving toward stall by decreasing the equivalent rotor speeds while the pressure ratio remained approximately constant. Stall originated as a rotating zone in the low-pressure compressor which resulted as a terminal stall in the high-pressure compressor. Decreasing the Reynolds number index to 0.25 from 0.5 reduced the required distortion for stall by 50 percent for the conditions investigated

    Combined pressure and temperature distortion effects on internal flow of a turbofan engine

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    An additional data base for improving and verifying a computer simulation developed by an engine manufacturer was obtained. The multisegment parallel compressor simulation was designed to predict the effects of steady-state circumferential inlet total-pressure and total-temperature distortions on the flows into and through a turbofan compression system. It also predicts the degree of distortion that will result in surge of the compressor. The effect of combined 180 deg square-wave distortion patterns of total pressure and total temperature in various relative positions is reported. The observed effects of the combined distortion on a unitary bypass ratio turbofan engine are presented in terms of total and static pressure profiles and total temperature profiles at stations ahead of the inlet guide vanes as well as through the fan-compressor system. These observed profiles are compared with those predicted by the complex multisegment model. The effects of relative position of the two components comprising the combined distortion on the degree resulting in surge are discussed. Certain relative positions required less combined distortion than either a temperature or pressure distortion by itself

    Performance and stall limits of a YTF30-P-1 turbofan engine with uniform inlet flow

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    Performance and stall limits of YTF30-P-1 turbofan engine with uniform compressor inlet flo

    Summary of recent investigations of inlet flow distortion effect on engine stability

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    A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression systems. Circumferential distortions of pressure and temperature, separately and in combination are considered. Resulting engine sensitivity measurements are compared with predictions based on simplified parallel compressor models and with several distortion descriptor parameters

    Effects of normative and informational social influence on visitor behavior in occupied grizzly bear habitat

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    The development and optimization of a hydrogen-fueled internal combustion engine

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    Conventional internal combustion engines modified to burn hydrogen fuel offer a good transition mode to a hydrogen economy for transportation applications. Details are given about the development of one such approach. This effort starts with a conventional 454 cubic inch Chevrolet V-8 engine that is then modified in various ways to accommodate the use of hydrogen; including specially formed intake and exhaust passages, modified cam, and fuel injection. Because the application is for constant speed application, tuned intake and exhaust is used

    Summary of investigations of engine response to distorted inlet conditions

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    A survey is presented of experimental and analytical experience of the NASA Lewis Research Center in engine response to inlet temperature and pressure distortions. This includes a description of the hardware and techniques employed, and a summary of the highlights of experimental investigations and analytical modeling. Distortion devices successfully simulated inlet distortion, and knowledge was gained about compression system response to different types of distortion. A list of NASA research references is included
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