ScholarLens Back to search
1949•NASA STI Repository (National Aeronautics and Space Administration)Open access

Comparison of the Aerodynamic Characteristics of the NACA 0010 and 0010-64 Airfoil Sections at High Subsonic Mach Numbers

Perry P Polentz

Open full text 2 citations

Abstract

coefficients up to 0.4, but the rate of drag rise above the Mach number for drag divergence was notappreciablychanged.Pitching moment was affected to a negligible degree.

Open-access reader

About this research paper

What this paper is about

coefficients up to 0.4, but the rate of drag rise above the Mach number for drag divergence was notappreciablychanged.Pitching moment was affected to a negligible degree.

Why it matters

OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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

coefficients up to 0.4, but the rate of drag rise above the Mach number for drag divergence was notappreciablychanged.Pitching moment was affected to a negligible degree.

Key concepts: Airfoil, Aerodynamics, Mach number, Pitching moment, NACA airfoil, Reynolds number, Drag divergence Mach number, Drag

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Comparison of the Aerodynamic Characteristics of the NACA 0010 and 0010-64 Airfoil Sections at High Subsonic Mach Numbers — Research Paper | ScholarLens