ScholarLens Back to search
1957•NASA STI Repository (National Aeronautics and Space Administration)Open access

Wind-tunnel investigation at high subsonic speeds of the effects on static stability characteristics of various modifications to a swept-wing fighter-type airplane model

Kenneth W Goodson

Open full text 0 citations

Abstract

Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model

Open-access reader

About this research paper

What this paper is about

Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model

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

Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model

Key concepts: Airplane, Wing, Aerospace engineering, Wind tunnel, Stability (learning theory), Longitudinal static stability, Aerodynamics, Wing loading

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Wind-tunnel investigation at high subsonic speeds of the effects on static stability characteristics of various modifications to a swept-wing fighter-type airplane model — Research Paper | ScholarLens