2007
DOI: 10.2514/1.26830
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Tradeoffs in Jet Inlet Design: A Historical Perspective

Abstract: The design of the inlet(s) is one of the most demanding tasks of the development process of any gas turbine-powered aircraft. This is mainly due to the multi-objective and multidisciplinary nature of the exercise. The solution is generally a compromise between a number of conflicting goals and these conflicts are the subject of the present paper. We look into how these design tradeoffs have been reflected in the actual inlet designs over the years and how the emphasis has shifted from one driver to another. We… Show more

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Cited by 51 publications
(34 citation statements)
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“…The exit dynamic pressure (q e ) is calculated by first assuming an exit area and a discharge coefficient. The discharge coefficient itself depends on the exit to inlet dynamic pressure ratio and the flow exit angle [6]. The flow exit angle is assumed to be 30°f or which _ m = 0.827 kg/s and n = 0.14.…”
Section: Aspects Of Oil Cooler Duct Designmentioning
confidence: 99%
“…The exit dynamic pressure (q e ) is calculated by first assuming an exit area and a discharge coefficient. The discharge coefficient itself depends on the exit to inlet dynamic pressure ratio and the flow exit angle [6]. The flow exit angle is assumed to be 30°f or which _ m = 0.827 kg/s and n = 0.14.…”
Section: Aspects Of Oil Cooler Duct Designmentioning
confidence: 99%
“…4 However, a large number of aircraft do not use this approach even though it is an idea that has been around well before they were created. 8 For example, both the Vought F-8 Crusader and the General Dynamics F-16 both use fixed normal shock inlets. At first glance, it may appear that the designers were trying to save on cost and keep the simple, cheaper inlet design.…”
Section: Introductionmentioning
confidence: 99%
“…It creates excessive vibrations in tall buildings and other wind‐sensitive structures, thus increasing the risks of losing their structural integrity . In case of an aircraft engine, wind (especially the crosswind) modifies interaction of the airflow with engine inlet structures, where geometry of the intake defines parameters of the airflow ingested by the engine and resistance to flow separation at varying operational conditions …”
Section: Introductionmentioning
confidence: 99%