Experimental Investigation of the Separated Flow Past Slender Bodies in the RAE 5 Metre Low-Speed Pressurised Wind Tunnel
Abstract
Tests carried out on a cone-cylinder model in the 5 metre low-speed wind tunnel have provided examples of the pressure distribution near the nose in conditions where significant values of side force occur, showing how this is dependent on roll angle of the nominally axially-symmetric body. At values of roll where the side force is at its maximum, comparison of the measured pressure distribution with that predicted theoretically, using an inviscid mathematical model of the separated flow past a slender cone, shows that the major features of the flow are identified reasonably well by the inviscid model and that the development of the side force at least in its major features can be described without the need for appeal of any additional viscous interaction. Further work, however, will be necessary to identify the mechanisms giving rise to intermediate values of side force.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1991
- Accession Number
- ADA236527
Entities
People
- D. E. Lean
- I. R. Moir
- S. P. Fiddes
Organizations
- Royal Aircraft Establishment