by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English
|Statement||J.P. Kreskovsky, W.R. Briley, and H. McDonald ; prepared for Lewis Research Center under contract NAS3-20951.|
|Series||NASA contractor report -- 3494., NASA contractor report -- NASA CR-3494.|
|Contributions||Briley, W. R., McDonald, H. 1937-, Lewis Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Scientific Research Associates.|
|The Physical Object|
Get this from a library! Turbofan forced mixer-nozzle internal flowfield. [J P Kreskovsky; W R Briley; H McDonald; Lewis Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Scientific Research Associates.]. Turbofan forced mixer-nozzle internal flowfield Volume of NASA contractor report Turbofan Forced Mixer-nozzle Internal Flowfield, M. J. Werle: Authors: M. J. Werle, V. N. Vatsa, United Technologies Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch: Publisher. three-dimensional flowfield development within the lobe region of turbofan forced mixer nozzles. The study represents a continuation of an effort initiated by NASA and UTRC in to develop computational procedures for predicting forced mixer File Size: 4MB. Turbofan Forced Mixer-Nozzle Internal Flowfield II - Computational Fluid Dynamic Predictions M. J. Werle and V. N. Vatsa United Techno Zogies Research Center East Hartford, Connecticut Prepared for Lewis Research Center under Contract NAS 1 National Aeronautics and Space Administration Scientific and Technical.
If further mesh node Turbofan forced mixer/nozzle temperature and flow field modelling lobed mixer exit plane (mixing plane) mixing duct exit FIG. 2. Geometry of lobed mixer, downstream mixing duct and separate solution domains. increases were to be made, it is the R-G mesh which would be worthwhile of further by: Numerical investigation of lobe spacing ratio on performance of forced mixer nozzle Article in Heat Transfer-Asian Research 40(7) November with 15 Reads How we measure 'reads'. LDV Measurement of Confined Parallel Jet Mixing Robert F. Kunz, Robert F. Kunz. Lockheed Martin, Schenectady, NY Patrick, R. W., , “Flowfield Measurements in a Separated and Reattached Flat Plate Turbulent Boundary Layer,” NASA CR, March. , “Turbofan Forced Mixer-Nozzle Internal Flowfield, I-Benchmark Cited by: 9. Experimental Studies of Flow Fields in Internal Combustion Engines Turbofan forced mixer-nozzle internal flowfield. Volume 1: A benchmark experimental study.
Paterson, R W. Turbofan Forced Mixer-Nozzle Internal Flowfield, Part 1: A Benchmark Experimental Study. ASME Journal of Engineering for Gas Turbine Engines and Power, , – Article; Google ScholarAuthor: Suofang Wang, Liguo Li, Jingzhou Zhang. Abstract. In a continuing effort to study the mixing enhancement by large scale streamwise vortices generated by a lobed nozzle, a high-resolution stereoscopic PIV system was used in the present study to conduct three-dimensional measurements of air jet flows exhausted from a lobed nozzle and a conventional circular by: 3. Looking for DEVCON Mixing Nozzle, Mixing Ratio, ml Mix Nozzles Nozzle Type (4TT45)? Grainger's got your back. Price $ Easy online ordering for the ones who get it done along with 24/7 customer service, free technical support & : $ Forced Mixer & Nozzle Noise Reduction PWC2 Objectives: Determine the most noise influential parameters of mixer nozzles. Provide a design tool to optimize forced mixer and nozzle for performance (for Cruise) as well as noise (for Take-off and Approach).