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- W177592918 abstract "This Note describes an experimental investigation into the pressures over the base of two afterbody configurations, in the presence of jet streams issuing from sonic nozzles in the base. The tests were made over a range of Mach numbers from 0.8 to 1.3 in the R.A.E. 2 ft x 1 .5 ft transonic wind tunnel. A description is given of the plant which supplied air to the nozzles, together with the method of testing. One of the afterbody configurations was of constant square section with rounded corners, containing four symmetrically positioned sonic nozzles; three models of this configuration were tested, with nozzle area as the varying parameter. The other afterbody configuration was cylindrical with a central sonic nozzle; this model was included in the programme as a basis of comparison with other published work. The results of the tests covering the main experimental programme are presented in the form of curves of base pressure coefficient against jet pressure ratio, showing the separate effects of Mach number, jet/base area ratio and model length. Numerous schlieren photographs are included. These have been used to support a tentative explanation of the characteristics of the base pressure curves." @default.
- W177592918 created "2016-06-24" @default.
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- W177592918 date "1963-02-28" @default.
- W177592918 modified "2023-09-26" @default.
- W177592918 title "A base pressure investigation, at transonic speeds, on an afterbody containing four sonic nozzles and a cylindrical afterbody containing a central sonic nozzle" @default.
- W177592918 hasPublicationYear "1963" @default.
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