ScholarLens Back to search
1967•NASA STI Repository (National Aeronautics and Space Administration)Open access

Aerodynamics of the model airplane. Part 1 - Airfoil measurements

Frédéric Schmitz

Open full text 29 citations

Abstract

Airfoil measurements that show behavior of wing sections in low-turbulence stream in Reynolds number range from 20,000 to 170,000

Open-access reader

About this research paper

What this paper is about

Airfoil measurements that show behavior of wing sections in low-turbulence stream in Reynolds number range from 20,000 to 170,000

Why it matters

OpenAlex reports 29 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

Airfoil measurements that show behavior of wing sections in low-turbulence stream in Reynolds number range from 20,000 to 170,000

Key concepts: Airplane, Airfoil, Aerodynamics, Aerospace engineering, Aeronautics, Computer science, Engineering

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Aerodynamics of the model airplane. Part 1 - Airfoil measurements — Research Paper | ScholarLens