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Naca 0015

Naca 0015 is described in multiple online sources, as addition to our editors' articles, see section below for printable documents, Naca 0015 books and related discussion.

Suggested Pdf Resources

Numerical simulation of lift enhancement on a NACA 0015 airfoil
configuration is a NACA 0015 airfoil with a ZNMF jet normal to the surface, .
NACA0015 Measurements in LM Wind Tunnel and Turbulence
Abstract (max. 2000 char.
UNSTEADY MULTIPHASE MODELING OF CAVITATION AROUND
cavitation around the NACA 0015. The unsteady cavitation around NACA 0015 is investigated.
LES Simulations of NACA0015 Hydrofoil
LES Simulations of NACA0015 Hydrofoil. Combustion Research and Flow Technology, Inc.
MODELING OF CAVITATION FLOW ON NACA 0015 HYDROFOIL
ON NACA 0015 HYDROFOIL. Jaroslav Štigler*, Jan Svozil*. This paper is concerning with simulations of cavitation flow around the NACA 0015 hydrofoil.

Suggested News Resources

WESMAR to Introduce New Fin for Yachts
The fin shape used is to NACA 0015 standard fin profile and provides optimum lift to drag ratios and geometric size.

Suggested Web Resources

NACA airfoil - Wikipedia, the free encyclopedia
The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA).
Airfoil Investigation Database - Showing NACA 0015
Jan 22, 2011 Quick search for an airfoil. Browse | Search | Compare | Templates | About. NACA 0015.
NACA0015 LIFT DATA
AIRFOIL: NACA 0015. DATA: Lift Coefficients ------------------------------------------------ --------------------- ORIGINAL SOURCE: Sheldahl, R. E.
Numerical simulation of lift enhancement on a NACA 0015 airfoil
configuration is a NACA 0015 airfoil with a ZNMF jet normal to the surface, .
Naca 0015
i believe NACA0015 means 0 camber at the leading point of the airfoil and having 15% thickness of the chord line......

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