Procedures were developed for making aerodynamic models of parallel continuous channels, an arrangement often involved in metallurgy and power engineering, together with experimentation procedures for the models obtained. The procedures enable fabrication of models to be simplified and experimentation under laboratory conditions made easier.
NASA STI/Recon Technical Report N
- Pub Date:
- November 1984
- Channel Flow;
- Flow Characteristics;
- Bernoulli Theorem;
- Fluid Mechanics and Heat Transfer