Work

NASA supercritical airfoils: A matrix of family-related airfoils

Year: 1990

Type: article

Abstract: The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented.

Source: NASA STI Repository (National Aeronautics and Space Administration)

Author: C. D. Harris

Institution: Langley Research Center

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W1519288965

FWCI: 0.539

Cites:

Cited by: 109

Related to: 10