1951•NASA Technical Reports Server (NASA)Requires access

Investigation of the effects of leading-edge chord-extensions on the aerodynamic and control characteristics of two sweptback wings at Mach numbers 1.41, 1.62, and 1.96

B May Ellery

Open publisher page 1 citations

Abstract

This record does not include an abstract. Use the full-text link above if available.

About this research paper

What this paper is about

An abstract is not available in the OpenAlex record for this paper.

Why it matters

OpenAlex reports 1 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.

Key concepts: Chord (peer-to-peer), Aerodynamics, Mach number, Leading edge, Computer science, Aerospace engineering, Engineering, Distributed computing

Back to paper search Browse research topics Original source

Investigation of the effects of leading-edge chord-extensions on the aerodynamic and control characteristics of two sweptback wings at Mach numbers 1.41, 1.62, and 1.96 — Research Paper | ScholarLens