A numerical simulation of the NFAC (National Full-scale AerodynamicsComplex) open-return wind tunnel inlet flow
Author(s) -
Upender K. Kaul,
John Ross,
J. L. Jacocks
Publication year - 1985
Publication title -
23rd aerospace sciences meeting
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1985-437
Subject(s) - inlet , wind tunnel , marine engineering , scale (ratio) , flow (mathematics) , return flow , computer simulation , environmental science , meteorology , mechanics , computer science , aerospace engineering , geology , simulation , engineering , physics , geomorphology , quantum mechanics
The flow into an open return wind tunnel inlet was simulated using Euler equations. An explicit predictor-corrector method was employed to solve the system. The calculation is time-accurate and was performed to achieve a steady-state solution. The predictions are in reasonable agreement with the experimental data. Wall pressures are accurately predicted except in a region of recirculating flow. Flow-field surveys agree qualitatively with laser velocimeter measurements. The method can be used in the design process for open return wind tunnels.
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom