ScholarLens Back to search
2008•Aeronautical Computing TechniqueRequires access

Aerodynamic Design of Flying-wing UCAV

Bai Junqiang

Open publisher page 0 citations

Abstract

Since flying-wing configuration has excellent performance in aerodynamic,stealth capability and structure,it has become an ideal configuration of the future UCAV.An UCAV of 20t take-off weight,2t payload and 5000km range with a cruising Mach of 0.7 is designed.By using the Euler equation solver and viscosity amending,the aerodynamic performance is calculated and improved.The coefficient K and the moment performance are ameliorated.The result shows that the thought of this paper is feasible.

About this research paper

What this paper is about

Since flying-wing configuration has excellent performance in aerodynamic,stealth capability and structure,it has become an ideal configuration of the future UCAV.An UCAV of 20t take-off weight,2t payload and 5000km range with a cruising Mach of 0.7 is designed.By using the Euler equation solver and viscosity amending,the aerodynamic performance is calculated and improved.The coefficient K and the moment performance are ameliorated.The result shows that the thought of this paper is feasible.

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

Since flying-wing configuration has excellent performance in aerodynamic,stealth capability and structure,it has become an ideal configuration of the future UCAV.An UCAV of 20t take-off weight,2t payload and 5000km range with a cruising Mach of 0.7 is designed.By using the Euler equation solver and viscosity amending,the aerodynamic performance is calculated and improved.The coefficient K and the moment performance are ameliorated.The result shows that the thought of this paper is feasible.

Key concepts: Aerodynamics, Aerospace engineering, Wing, Payload (computing), Mach number, Euler equations, Euler angles, Solver

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Aerodynamic Design of Flying-wing UCAV — Research Paper | ScholarLens