ScholarLens Back to search
2009•Moscow University Mechanics BulletinRequires access

Supersonic flow around a body of small elongation

Sergey Vladimirovich Guvernyuk, Alexander F. Zubkov, Konstantin M. Pichkhadze, V. S. Finchenko, A. I. Shvets

Open publisher page 0 citations

Abstract

Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.

About this research paper

What this paper is about

Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.

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

Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.

Key concepts: Mach number, Drag, Mechanics, Elongation, Angle of attack, Lift (data mining), Supersonic speed, Static pressure

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Supersonic flow around a body of small elongation — Research Paper | ScholarLens