(:5) An investigation of the extent to which the boundary layers and tip clearances affect the performance of the unit. and ... case In the model (0-17(agt; scale) the arrangement has been simplified by the removal of the engine and nacelle at the rear of the ... Outline diagram of duct and fans The test was carried out in the O.S.I.R. 9a#39; x 7a#39; closed atmospheric tunnel. ... by means of an electrical indicator to be described later. C.-MS6 4.w 3 Tost Ref. No. J. ! nit ft. sec. , ft. WIND TI.NNKI. TKS.
|Author||:||Australia. Dept. of Supply. Aeronautical Research Consultative Committee|