2 edition of Turbofan forced mixer-nozzle internal flowfield found in the catalog.
Turbofan forced mixer-nozzle internal flowfield
Robert W. Paterson
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||Robert W. Paterson ; prepared for Lewis Research Center under contract NAS3-20951.|
|Series||NASA contractor report -- 3492., NASA contractor report -- NASA CR-3492.|
|Contributions||Lewis Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., United Technologies Research Center.|
|The Physical Object|
Implementation of Benchmarking Transportation Logistics Practices and Future Benchmarking Organizations. SciTech Connect. Thrower, A.W.; Patric, J.; Keister, M. the 3 D physical space in the objective fluid flow and the image planes of the cameras used for stereoscopic image recording. The flow chart to reconstruct the three components of the velocity vectors in the measurement plane of phys- ical space from the 2D displacement vectors detected by the two cameras is also given.
Werle, M. J. Turbofan forced mixer-nozzle internal flowfield / M.J. Werle and V.N. Vatsa ; prepared for Lewis Research Center under contract NAS Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.: For sale by the National Technical Information Service], Machine mixer nozzle type Is with advantage used when the machine's (the screw's) mixer isn't efﬁ cient enough or when you wish a even better after-mixing result. The totally large ﬂ ow-way results in a low pressure loss and a very good mixer effect. At the same time the nozzle has a built in ﬁ l-.
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The item Turbofan forced mixer-nozzle internal flowfield, M.J. Werle and V.N. Vatsa ; prepared for Lewis Research Center under contract NAS represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.
Turbofan forced mixer-nozzle internal flowfield. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.: For sale by the National Technical Information Service], (OCoLC) Material Type: Government publication, National government publication: Document Type.
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. Werle: Authors: M. Werle, V.
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. Werle and V. 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. 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.
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Volume 2: Computational fluid dynamic predictions. NASA Technical Reports Server (NTRS) Werle, M. J.; Vasta, V. A general program was conducted to develop and assess a computational method for predicting the flow properties in a turbofan forced mixed duct.
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