ScholarLens Back to search
Year unknown•NASA STI Repository (National Aeronautics and Space Administration)Open access

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01

Carlson, H. W.

Open full text 0 citations

Abstract

Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wing-body combinations

Open-access reader

About this research paper

What this paper is about

Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wing-body combinations

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

Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wing-body combinations

Key concepts: Fuselage, Mach number, Wing, Flow (mathematics), Mechanics, Mathematics, Aerospace engineering, Physics

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 — Research Paper | ScholarLens