1966NASA Technical Reports Server (NASA)Requires access

Effect of wing leading-edge shape on aerodynamic characteristics of a 67 deg swept wing-body model at Mach 1.50 to 4.63

M. O. Feryn, R. G. Kyle

Open publisher page 0 citations

Abstract

Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63

About this research paper

What this paper is about

Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63

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

Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63

Key concepts: Wing, Aerodynamics, Leading edge, Wing twist, Mach number, Swept wing, Wing configuration, Wing loading

Related papers

Back to paper searchBrowse research topicsOriginal source
Effect of wing leading-edge shape on aerodynamic characteristics of a 67 deg swept wing-body model at Mach 1.50 to 4.63 — Research Paper | ScholarLens