1953•NASA Technical Reports Server (NASA)Requires access

An investigation of the transonic area rule by flight tests of a sweptback wing on a cylindrical body with and without body indentation between Mach numbers 0.9 and 1.8

Sherwood Hoffman

Open publisher page 2 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 2 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: Transonic, Mach number, Wing, Aerospace engineering, Aeronautics, Engineering, Acoustics, Structural engineering

Back to paper search Browse research topics Original source

An investigation of the transonic area rule by flight tests of a sweptback wing on a cylindrical body with and without body indentation between Mach numbers 0.9 and 1.8 — Research Paper | ScholarLens