Work

A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness

Year: 1953

Type: article

Authors: W L Gray, K M Schenk

Institution: Boeing (United States)

Language: English

Topic: Aeroelasticity and Vibration Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W351320895

FWCI: 2.123

Cites:

Cited by: 26

Related to: 10