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Nasa Technical Reports Server (ntrs) 20150004420%3a Computational Fluid Dynamics Modeling Of A Supersonic Nozzle And Integration Into A Variable Cycle Engine Model by Nasa Technical Reports Server (ntrs)
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1NASA Technical Reports Server (NTRS) 20150004420: Computational Fluid Dynamics Modeling Of A Supersonic Nozzle And Integration Into A Variable Cycle Engine Model
By NASA Technical Reports Server (NTRS)
This paper covers the development of an integrated nonlinear dynamic simulation for a variable cycle turbofan engine and nozzle that can be integrated with an overall vehicle Aero-Propulso-Servo-Elastic (APSE) model. A previously developed variable cycle turbofan engine model is used for this study and is enhanced here to include variable guide vanes allowing for operation across the supersonic flight regime. The primary focus of this study is to improve the fidelity of the model's thrust response by replacing the simple choked flow equation convergent-divergent nozzle model with a MacCormack method based quasi-1D model. The dynamic response of the nozzle model using the MacCormack method is verified by comparing it against a model of the nozzle using the conservation element/solution element method. A methodology is also presented for the integration of the MacCormack nozzle model with the variable cycle engine.
“NASA Technical Reports Server (NTRS) 20150004420: Computational Fluid Dynamics Modeling Of A Supersonic Nozzle And Integration Into A Variable Cycle Engine Model” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20150004420: Computational Fluid Dynamics Modeling Of A Supersonic Nozzle And Integration Into A Variable Cycle Engine Model
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 20150004420: Computational Fluid Dynamics Modeling Of A Supersonic Nozzle And Integration Into A Variable Cycle Engine Model” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - COMPUTATIONAL FLUID DYNAMICS - NONLINEARITY - DYNAMIC MODELS - SUPERSONIC NOZZLES - TURBOFAN ENGINES - SERVOMECHANISMS - THRUST - FLOW EQUATIONS - CONVERGENT-DIVERGENT NOZZLES - VARIABLE CYCLE ENGINES - MATHEMATICAL MODELS - NOZZLE DESIGN - SIMULATION - CONSERVATION EQUATIONS - CHOKED FLOW - Connolly, Joseph W. - Friedlander, David - Kopasakis, George
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_20150004420
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 22.81 Mbs, the file-s for this book were downloaded 69 times, the file-s went public at Fri Nov 18 2016.
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