The effects of Reynolds number, Mach number, and gas species (air and CO 2) on
aerodynamic characteristics of a thin flat plate and a NACA 0012-34 airfoil were investigated …

The flowfields around the NACA 0012 airfoil at Reynolds numbers 1× 10 4, 3× 10 4, and 5×
10 4 are studied, and the predictability of aerodynamic characteristics derived from various …

A high-performance Ishii airfoil was analyzed using both a wind-tunnel and large-eddy
simulations at a low-Reynolds-number condition (R e= 23,000). The design guidelines for …

This work investigates the aerodynamics of a NACA 0012 airfoil at the chord-based
Reynolds numbers (Re c) from 5.3× 10 3 to 2.0× 10 4. The lift and drag coefficients, CL and …

I. Introduction wide range of engineering devices employ airfoils operating at relatively low
chord Reynolds numbers. Specifically, airfoil performance in the chord Reynolds number …

In this study, the flowfields around NACA0012 and NACA0002 airfoils at Reynolds number
of 23,000 and the aerodynamic characteristics of these flowfields were analyzed using …

THE need for cost-effective high-altitude vehicles to conduct atmospheric research has
created interest in high-altitude (low Reynolds number) airfoils. In support of this need …

OW-Reynolds-number aerodynamics is important for both military and civilian applications.
These applications include propellers, sailplanes, ultra-light man-carrying/man-powered …

THE flow properties in the low-Reynolds-number range, which are applicable to small-sized
aerovehicles, wind turbines, propellers, and human-powered aerovehicles, have generally …

Presented in this report is a description of a test program conducted in the Langley Low-
Turbulence Pressure Tunnel to produce the low-speed aerodynamic characteristics of the …