International Journal of Aerospace Engineering / 2009 / Article / Fig 11

Research Article

Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

Figure 11

Initial and final airfoil sections and Mach number distributions for streamline between the nozzle tip and pitch [SL 5].

We are committed to sharing findings related to COVID-19 as quickly and safely as possible. Any author submitting a COVID-19 paper should notify us at to ensure their research is fast-tracked and made available on a preprint server as soon as possible. We will be providing unlimited waivers of publication charges for accepted articles related to COVID-19. Sign up here as a reviewer to help fast-track new submissions.