From: Richard Noble Sent: 17 July 1996 21:17 To: Desmond Weller Subject: RE: American Eagle's thoughts Hi Desmond, Look I can't speak for the other teams since I just don't know what their level of research is and hence their ability to address the supersonic issues with credibility. So I can only respond for us: We set out to achieve the first ever supersonic car- thats why our car is called ThrustSSC and why the logo shows the supersonic shock on the nose. In otherwords we are attempting to achieve the first ever supersonic run -and we are not just a land speed record car. When I drove T2 to the record in 1983,frankly as a team we were damned lucky to get away with it. The car was within 7 mph of takeoff and with the huge dynamic pressures involved it would have gone upwards at 40G. When we learned of Breedloves new car, we decided that this was just the sort of competitive impetus we required to enable us fund the supersonic car and carry out the 2.5 years of research. It is important to understand that when we started the research phase Ron Ayers (ex Chief Aerodynamicist - Guided Weapons - BAC) and I were very concerned that we might end up building another intuitive and possibly highly dangerous car. We therefore agreed that unless the the research phase demonstrated that car were safe, we would not proceed and if the car became dangerous at any time, we would withdraw. When we started the research , we were unable to find anyone with any relevant experience. We therefore created our own using two untried and unproven methods of evaluation. The Flite CFD software has been extensively validated for aircraft but never for ground based vehicles. The Pendine rocket test track has been used for missile and bomb development- never for supersonic land vehicle modelling. At the start of the programme which would compare identical cases on CFD and with the live rocket modelling, Ron made it quite clear to me (and I had to pass this on to Castrol) that he believed there was only a 10% chance of getting any kind of meaningful correlation between results from the two untried and unvalidated methods of test. If the results did not match then,we would not know which to believe (if either). If the results did match, they might show an unfavourable and hostile airflow. Only if the results matched and showed a favourable result would Ron consider continuing with the programme. The results of the two year programme were extraordinarily conclusive and Ron had the results independantly audited by the TI Group who sent two Dowty aerospace engineers to check and report. On this basis Ron felt happy to proceed and in that case so did I. Whilst we are out on the desert making high speed runs thanks to Kulite Hughes and the University of Swansea, using Jerry Bliss'tremendous data acquisition capability, we can measure and record the airflow plot under the full scale car for any mach no on any run. This means we are able to use that fullscale data- send it back to Swansea for further CFD on their Cray computer and compare it with the very extensive modelling data we have already amassed. It thus becomes possible to predict the airflow under/over the car using the CFD modelling and basing it on our research. For the first time , instead of driving Thrust 2 into the blue as I did in 1983, it now becomes possible to evaluate each stage of the aerodynamic performance in advance of the run- and to crosscheck it after the run. I'd like you to understand that as a team we are all committed to achieving this and enormous effort has gone into the development and creation of ThrustSSC because we believe we can do it. And you can follow all this on the net as we start to put the theory into practice. When we started , we found plenty of highly qualified aerodynamicists who told us that a supersonic land vehicle was highly dangerous and could never be done in safety. When we cross examined them we inevitably found that their arguement was based on their experience, which did not include on the ground supersonic vehicles. Its a free World- there are plenty of Cray 92 computers and rocket test tracks around. Anyone can go out and flog through 2.5 years of tough demanding and very difficult to finance research. Only when you have done that should you venture to express an opinion and expect any credibility. Many thanks for your interest and for following ThrustSSC. Richard Noble.
Sponsored by | This site best viewed with Microsoft Internet Explorer 3 | |||