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Can anyone here comment on the kinds of things you can and can't learn accurately from a scaled prototype? I'd guess that for something that flies, changing the
by abeppu 6y ago
Can anyone here comment on the kinds of things you can and can't learn accurately from a scaled prototype? I'd guess that for something that flies, changing the surface area/volume ratio makes a big difference.
- redis_mlc 6y agoI study aerodynamics, and haven't heard of problems from scaling down the models. The main problem with supersonic wind tunnels is ensuring there's no interference from shock waves bouncing off the sides of the tunnel, which is why the X-plane program used actual airplanes. So wind tunnels are rated to a certain Mach, and above that, like for hypersonic, actual airplanes are still used. FYI: I believe the DC-3 was the first passenger airplane designed with a wind tunnel, and as a result was efficient enough to be the first twin-engine commercial passenger airplane to fly over the Rockies with a safety margin to fly single-engine, and adequate to be the first proposed Shuttle wing design.
- starpilot 6y agohttps://i2.cdn.turner.com/money/dam/assets/170324152006-boom-aerospace-supersonic-xb-1-780x439.jpg https://i2.cdn.turner.com/money/dam/assets/170324152006-boom... This is a tech demonstrator and not quite a "scaled prototype." Two occupants vs ~40 makes it pretty much a completely different aircraft. What it's probably demonstrating is some key design aspects like inlet/engine interactions, sonic boom mitigation, thermal resistance on various points, and overall validating simulation data. It won't show anything about extrinsic performance like range or takeoff distance of the final passenger jet, at least not directly.
- jazzyjackson 6y agoWell you can use the same materials and manufacturing process that you intend to use for the full scale model, and know that your carbon composite body holds up as good as the simulations.
- na85 6y agoIn aerodynamics we have several "similarity" quantities such as the Reynolds Number which is a dimensionless coefficient that characterizes (in a nutshell) the ratio of inertial to viscous forces in a flow. Much research has gone into the applicability of scale models to real world conditions and the validity of a model is contingent on maintaining similarity coefficients. So for example you want your model to be flying at the same Reynolds Number as your full size aircraft will. If you can achieve those conditions then you can expect good predictive results from your model. In general you can learn a great deal about your aircraft from a model including handling and stability characteristics but you're limited by the tunnel and the test apparatus. Post stall behavior comes to mind as something I would imagine to be very difficult to investigate with a scale model in a tunnel.
- fluffy87 6y agoTheir half-size model would need to be flying twice as fast for the Reynolds number to remain constant with varying length or diameter. This changes the Mach number. So no, in general, you can’t build and test a smaller model and transfer the results to a larger model using similarity, because your similarity model is incomplete. You can either have similarity for the Reynolds number or the Mach number, but not both.
- bluGill 6y agoThe unknown unknowns. There is always something you forgot to account for. So you do many different models and then a few full sized prototypes to give you the best chance of finding everything.