ScholarLens Back to search
1941•NASA Technical Reports Server (NASA)Open access

Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps

Marvin J Schuldenfrei

Open full text 0 citations

Abstract

In q~n~r~l,under comparable conditions, the provl -OUSIF i!.ovolopod Elottcd flnp had oqunl or so=owhat lower pltchinq-nomont coefficients than either size of balanced split fla>.-Go to the stall.

Open-access reader

About this research paper

What this paper is about

In q~n~r~l,under comparable conditions, the provl -OUSIF i!.ovolopod Elottcd flnp had oqunl or so=owhat lower pltchinq-nomont coefficients than either size of balanced split fla>.-Go to the stall.

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

In q~n~r~l,under comparable conditions, the provl -OUSIF i!.ovolopod Elottcd flnp had oqunl or so=owhat lower pltchinq-nomont coefficients than either size of balanced split fla>.-Go to the stall.

Key concepts: Airfoil, NACA airfoil, Wind tunnel, Chord (peer-to-peer), Aerodynamics, Structural engineering, Geology, Engineering

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps — Research Paper | ScholarLens