Design of a sub-scale fan for a boundary layer ingestion test with by-pass flow

Abstract

A design of a sub-scale Boundary Layer Ingestion (BLI) fan for a transonic test rig is presented. The fan is intended to be used in flow conditions with varying distortion patterns representative of a BLI application on an aircraft. The sub-scale fan design is based on a design study of a full-scale fan for a BLI demonstration project for a Fokker 100 aircraft. CFD results from the full-scale fan design and the ingested distortion pattern from CFD analyses of the whole aircraft are used as inputs for this study. The sub-scale fan is designed to have similar performance characteristics to the full-scale fan within the capabilities of the test facility. The available geometric rig envelope in the test facility necessitates a reduction in geometric scale and consideration of the operating conditions. Fan blades and vanes are re-designed for these conditions in order to mitigate the effects of the scaling. The effects of reduced size, increased relative tip clearance and thicknesses of the blades and vanes are evaluated as part of the step-by-step adaption of the design to the sub-scale conditions. Finally, the installation effects in the rig are simulated including important effects of the by-pass flow on the running characteristics and the need to control the effective fan nozzle area in order to cover the available fan operating range. The predicted operating behaviour of the fan as installed in the coming transonic test rig gives strong indication that the sub-scale fan tests will be successful.

An altitude capable rig for studying engine inlet velocity profile effects: Boundary layer generator

“…Figure 14 shows velocity profiles at the fan inlet face of the Fokker 100 aircraft at its aerodynamic design point [11,12]. This data are taken from the CFD analysis of the whole aircraft including the tail-cone thruster [18].…”

“…The fan is about 1/7 scale and measures 18cm in tip diameter. The initial fan to be tested is designed for a distortion pattern of a fan mounted on the tail cone of an aircraft [11,12] and is mounted within a scaled nacelle (Fig. 4).…”

Effects of distortion on a BLI fan

“…An upstream centrebody allows different levels and patterns of distortion to be generated for building knowledge and validation. The design of the rig is described in more detail in (11) and the design of the test fan for use in the rig in [12]. The BLI distortion pattern used for this study includes both an axisymmetric radial variation as well as circumferential features.…”