1952•NASA STI Repository (National Aeronautics and Space Administration)Requires access

Wind-tunnel investigation at high and low subsonic Mach numbers of a thin sweptback wing having an airfoil section designed for high maximum lift

Stanley F Racisz, Nicholas J Paradiso

Open publisher page 3 citations

Abstract

This record does not include an abstract. Use the full-text link above if available.

About this research paper

What this paper is about

An abstract is not available in the OpenAlex record for this paper.

Why it matters

OpenAlex reports 3 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.

Key concepts: Airfoil, Wing, Lift (data mining), Mach number, Section (typography), Wind tunnel, Aerodynamics, Subsonic and transonic wind tunnel

Back to paper search Browse research topics Original source

Wind-tunnel investigation at high and low subsonic Mach numbers of a thin sweptback wing having an airfoil section designed for high maximum lift — Research Paper | ScholarLens