Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds
Willard G Smith, Louis H Ball
Abstract
Open-access reader
Willard G Smith, Louis H Ball
Abstract
Open-access reader
Wind tunnel tests to determine lateral-directional stability of aircraft from transonic to supersonic speeds
OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Wind tunnel tests to determine lateral-directional stability of aircraft from transonic to supersonic speeds
Key concepts: Airplane, Supersonic speed, Supersonic wind tunnel, Aerospace engineering, Longitudinal static stability, Wind tunnel, Stability (learning theory), Angle of attack