| 1250 |
 General guide to the choice of thrust bearing type. |
67033 |
| 1250 |
General guide to the choice of journal bearing type. |
65007 |
| 1250 |
ESDUview user manual. |
00009 |
| 1250 |
Tribology Series record of documents. |
00005 |
| 1250 |
Example of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Dual design point, upper and lower surface shape geometry, leading and trailing edge flap deflections, RAE 2822, Euler code and BVGK. |
01024 |
| 1250 |
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: single, geometry var: LE and TE flaps, initial aerofoil: combat aircraft section, CFD: BVGK (inviscid), Euler code. |
00023 |
| 1250 |
Example of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: single, geometry var: LE and TE flaps, initial aerofoil: combat aircraft section, CFD: BVGK (viscous flow) |
00022 |
| 1250 |
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: dual, geometry variation: LE and TE flap deflection and camber line vars, initial aerofoil: RAE 2822 |
99021 |
| 1250 |
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: single, geometry variation: LE and TE flap deflection or camber line vars, initial aerofoil: RAE 2822 |
99020 |
| 1250 |
Constrained multivariate optimisation techniques for the design of aerofoil sections. |
99019 |
