Damping in Yaw and Static Directional Stability of a Canard Airplane Model and of Several Models Having Fuselages of Relatively Flat Cross Section
Joseph L. Johnson
Abstract
Open-access reader
Joseph L. Johnson
Abstract
Open-access reader
This document contains classifi meaning of the Espionage Act, U manner to an unauthorized person i ' G Information so classified may b 2.
OpenAlex reports 1 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.
This document contains classifi meaning of the Espionage Act, U manner to an unauthorized person i ' G Information so classified may b 2.
Key concepts: Fuselage, Airplane, Longitudinal static stability, Cross section (physics), Wing, Stability (learning theory), Concentric, Structural engineering