1968NASA Technical Reports Server (NASA)Open access

Aerodynamic characteristics of a five jet VTOL configuration in the transition speed range

G. L. Gentry, R. J. Margason

Open full text 7 citations

Abstract

Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stability

Open-access reader

About this research paper

What this paper is about

Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stability

Why it matters

OpenAlex reports 7 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.

Available abstract

Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stability

Key concepts: Aerodynamics, Jet (fluid), Range (aeronautics), Mechanics, Aerospace engineering, Physics, Environmental science, Meteorology

Related papers

Back to paper searchBrowse research topicsOriginal source
Aerodynamic characteristics of a five jet VTOL configuration in the transition speed range — Research Paper | ScholarLens