ScholarLens Back to search
1965•Journal of AircraftRequires access

Numerical method of estimating and optimizing supersonic aerodynamic characteristics of arbitrary planform wings

WlLBUR D. MlDDLETON, H. W. Carlson

Open publisher page 27 citations

Abstract

Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics

About this research paper

What this paper is about

Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics

Why it matters

OpenAlex reports 27 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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

Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics

Key concepts: Aerodynamics, Planform, Supersonic speed, Wing, Aerospace engineering, Geology, Structural engineering, Swept wing

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Numerical method of estimating and optimizing supersonic aerodynamic characteristics of arbitrary planform wings — Research Paper | ScholarLens