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Journal ArticleDOI

Shock standoff distances and Mach-disk diameters in underexpanded sonic jets

W. Davidor, +1 more
- 01 Aug 1971 - 
- Vol. 9, Iss: 8, pp 1651-1653
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This article is published in AIAA Journal.The article was published on 1971-08-01. It has received 32 citations till now. The article focuses on the topics: Shock (mechanics) & Shock diamond.

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Citations
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Journal ArticleDOI

Free underexpanded jets in a quiescent medium: A review

TL;DR: In this article, the authors present an exhaustive overview of the main experimental papers dealing with underexpanded jets, from those where there is clearly a lack of confidence, and some clues are given on the numerical methods that may be used if one wants to study such jets numerically, together with an emphasis on the specific thermodynamic difficulties associated to this kind of extreme conditions.
Journal ArticleDOI

Scaling parameters for underexpanded supersonic jets

TL;DR: In this paper, a set of expressions were developed for afterexpansion equivalent jet exit diameter, velocity, temperature, and density to allow for a better collapse of jet spreading and centerline decay rates.
Journal ArticleDOI

Review on hydrogen safety issues: Incident statistics, hydrogen diffusion, and detonation process

TL;DR: In this article, the authors review the key issues concerning hydrogen safety, including hydrogen incident investigation, hydrogen leakage and diffusion, hydrogen ignition, and explosion, in combination with a practical survey analysis.
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Structure of Turbulent Sonic Underexpanded Free Jets

TL;DR: In this paper, the authors used laser-induced iodine flourescence and mean and fluctuating streamwise velocities using laser Doppler anemometry to predict turbulent mixing in fully developed pipe flows injected into still air.
References
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Journal ArticleDOI

On the Structure of Jets from Highly Underexpanded Nozzles Into Still Air

TL;DR: In this article, the position of the first normal shock in the jet behind a highly underexpanded nozzle is calculated using axial pressure distribution on the centerline of the flow behind the orifice, calculated by the method of characteristics, and the shock is then assumed to exist at that point where atmospheric pressure would be attained behind the shock.
Journal ArticleDOI

Viscous Hypersonic Flow Past a Slender Cone

K. Stewartson
- 01 May 1964 - 
TL;DR: In this paper, the strong interaction region in viscous hypersonic flow past a slender cone is considered and expressions for the pressure, shock, skin friction, and heat transfer are derived.