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- W2335706476 abstract "The integration of the airframe and its propulsion system is a key design issue in the development and deployment of military aircraft. The external airframe and inlet system must capture flow from the freestream and deliver it to the installed engine at Mach numbers commensurate with fan or compressor requirements. During aircraft maneuvers, the airflow to the engine becomes non-uniform or distorted. The aircraft developer and engine manufacturer must consider the compatibility of the inlet and the engine throughout the design process. The objective of the effort reported in this paper was to demonstrate an improved integrated test and evaluation (IT&E) capability that combines propulsion system numerical simulations (inlet-engine unsteady 3D aerodynamic codes) into the current test and evaluation process. The primary concern is to identify how to enhance the existing engine-inlet compatibility analysis and design methodology (ARP-1420) through the use of modeling and simulation (M&S) that integrates the aircraft and the propulsion system in a single computation process domain for the purpose of identifying system level improvements." @default.
- W2335706476 created "2016-06-24" @default.
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- W2335706476 date "2010-01-04" @default.
- W2335706476 modified "2023-10-01" @default.
- W2335706476 title "Demonstration of An Integrated Test and Evaluation(IT&E) Process for Airframe-Propulsion Systems Asapplied to A Current Weapon System Program" @default.
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- W2335706476 doi "https://doi.org/10.2514/6.2010-1039" @default.
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