ScholarLens Back to search
2013•TsAGI science journalRequires access

NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION

Sergey Mikhailovich Zadonsky, A. P. Kosykh, G. G. Nersesov, I. F. Chelysheva, S. V. Chernov, V. L. Yumashev

Open publisher page 1 citations

Abstract

Numerical simulation of inviscid flow over three hypersonic aircrafts of different idealized configurations with flow through the contoured duct of the air-jet engine has been performed at M∞ = 6 and α = 0−10°. The Influence of the front jaws of the air intake on the aerodynamic characteristics of the aircraft with a blunt wedged fuselage has been considered. The effect of different elements of the hypersonic aircraft on the aerodynamic characteristics has been estimated. Numerical data have been supplemented with the results of the experiments carried out in the wind tunnel at TsAGI.

About this research paper

What this paper is about

Numerical simulation of inviscid flow over three hypersonic aircrafts of different idealized configurations with flow through the contoured duct of the air-jet engine has been performed at M∞ = 6 and α = 0−10°. The Influence of the front jaws of the air intake on the aerodynamic characteristics of the aircraft with a blunt wedged fuselage has been considered. The effect of different elements of the hypersonic aircraft on the aerodynamic characteristics has been estimated. Numerical data have been supplemented with the results of the experiments carried out in the wind tunnel at TsAGI.

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.

Available abstract

Numerical simulation of inviscid flow over three hypersonic aircrafts of different idealized configurations with flow through the contoured duct of the air-jet engine has been performed at M∞ = 6 and α = 0−10°. The Influence of the front jaws of the air intake on the aerodynamic characteristics of the aircraft with a blunt wedged fuselage has been considered. The effect of different elements of the hypersonic aircraft on the aerodynamic characteristics has been estimated. Numerical data have been supplemented with the results of the experiments carried out in the wind tunnel at TsAGI.

Key concepts: Aerodynamics, Fuselage, Aerospace engineering, Hypersonic speed, Inviscid flow, Hypersonic flight, Wind tunnel, Duct (anatomy)

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION — Research Paper | ScholarLens