Airfoils

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Moshman Research has several technologies under development related to rotorcraft. For inquiries, please fill out our contact form.

Helicopter Acoustic Model (HAM) – A helicopter noise prediction tool that will be more accurate than the state-of-the-art FAA-approved tools and reduce expensive flight tests.

Blade Noise Reduction – A novel technique for eliminating the trailing pressure wake of an airfoil, thereby reducing noise significantly at transonic speeds.

High-Efficiency Blades – A novel technique for increasing lift and reducing drag at zero and negative angles of attack at transonic speeds.

Fire Suppression – A conceptual idea for increasing the spread of water coverage from fire helicopters in wild fire areas.