1982•NASA Technical Reports Server (NASA)Requires access

Low-speed aerodynamic characteristics of a 9.3-percent-thick supercritical airfoil section

Kevin W. Noonan, Robert McGhee

Abstract

An investigation was conducted in the Langley low turbulence pressure tunnel to determine the low-speed, two dimensional characteristics of a 9.3 percent-thick supercritical airfoil. The airfoil was tested at Reynolds numbers (based on chord) from 2.9 million to 16.8 million, at Mach numbers from 0.10 to 0.36, and at geometric angles of attack from -8 degrees to 14 degrees.

About this research paper

What this paper is about

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Key concepts: Airfoil, Chord (peer-to-peer), Mach number, Aerodynamics, Reynolds number, Turbulence, Mechanics, Drag divergence Mach number