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- W2042411687 abstract "The flow within an external target type thrust reverser is analyzed, using the simplifying assumptions that the flow is inviscid, incompressible, and two dimensional. The analysis is essentially an application of the freestreamline theory with numerical evaluation of integrals. In the analysis, a pair of transformations were used which allow the ejection angle to be expressed as a function of reverser geometric variables in two equations which have the form of improper integrals. These equations are then solved by numerical integration, with an approximation technique used at the singular points. Results are presented in the form of graphs which show the jet exit angle 0 as a function of the reverser geometric variables: L/e£, H/d, sweep angle, and endplate angle. Excellent agreement with test results from a twodimensional water jet is shown." @default.
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- W2042411687 date "1970-03-01" @default.
- W2042411687 modified "2023-09-27" @default.
- W2042411687 title "A mathematical model for the behavior of thrust reversers" @default.
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- W2042411687 doi "https://doi.org/10.2514/3.44141" @default.
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