ScholarLens Back to search
1955•NASA STI Repository (National Aeronautics and Space Administration)Open access

Experimental investigation at high subsonic speeds of the rolling-stability derivatives of a 1/22 scale model of the Republic F-105 airplane

W. C. Hayes, William C. Sleeman

Open full text 0 citations

Abstract

The derivatives of yawing moment and lateral force due to rolling generally followed trends indicated by previously published data.on a general research model.'.,I ___ ,__ ~ 7 .

Open-access reader

About this research paper

What this paper is about

The derivatives of yawing moment and lateral force due to rolling generally followed trends indicated by previously published data.on a general research model.'.,I ___ ,__ ~ 7 .

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

The derivatives of yawing moment and lateral force due to rolling generally followed trends indicated by previously published data.on a general research model.'.,I ___ ,__ ~ 7 .

Key concepts: Airplane, Scale (ratio), Stability (learning theory), Aerospace engineering, Engineering, Aeronautics, Mechanical engineering, Computer science

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Experimental investigation at high subsonic speeds of the rolling-stability derivatives of a 1/22 scale model of the Republic F-105 airplane — Research Paper | ScholarLens