Supersonic jets from bevelled rectangular nozzles

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .

Written in English

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  • Jet nozzles.

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Book details

StatementEdward J. Rice and Ganesh Raman.
SeriesNASA technical memorandum -- 106403.
ContributionsRaman, Ganesh., United States. National Aeronautics and Space Administration.
The Physical Object
Pagination1 v.
ID Numbers
Open LibraryOL17680108M

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Measured the noise produced by supersonic rectangular jets. Wlezien and Kibens 6 have conducted experiments on the noise generated by supersonic jets formed by round nozzles with unsymmetrical exits. One additional element found in the research reported here is that some of the nozzles are converging-diverging nozzles running nearlyFile Size: KB.

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SUPERSONIC JETS FROM BEVELLED RECTANGULAR NOZZLES Edward J. Rice* NASA Lewis Research Center Cleveland, Ohio Ganesh Raman** Sverdrup Technology Inc.

NASA Lewis Research Center Group Cleveland, Ohio ABSTRACT The influence of nozzle exit geometry on jet mixing and noise production was studied experimentally for a. Get this from a library. Screech tones of supersonic jets from bevelled rectangular nozzles.

[Christopher K W Tam; Hao Shen; Ganesh Raman; United States. National Aeronautics and Space Administration.]. In this paper, supersonic jets issuing from 30° and 60° bevelled nozzles were studied to investigate the influence of nozzle exit inclination upon the supersonic jet flow structures, particularly the shock cells within the jet potential core, at over-expanded, perfect expanded and under-expanded by: Supersonic jets at design Mach number of issuing from circular 30 deg and 60 deg double-beveled nozzles have been investigated experimentally and numerically in the present study, with a view to potentially improve mixing by: 4.

Flow characteristics of highly underexpanded jets at the same nozzle pressure ratio of but issuing from four different nozzles, i.e., the circular, elliptic, square, and rectangular nozzles. Time-resolved Schlieren photography-based image velocimetry using optical flow techniques (SIVOF) was applied to supersonic jet flows issued from a 30° bevelled nozzle.

Nozzles are actually used to modify the flow of a fluid (i.e. by increasing kinetic energy of the flow in expense of its pressure). Convergent-divergent type of nozzles are mostly used for supersonic flows because it is impossible to create supersonic flows (mach number more than one) in convergent type of nozzle and therefore it restricts us to a limited amount of mass flow through a.

Author of Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics, Time-domain impedance boundary conditions for computational aeroacoustics, Computational aeroacoustics, Direct computation of nonlinear acoustic pulses using high order finite difference schemes, Advances in numerical boundary conditions for computational.

A nozzle is a device designed to control the direction or characteristics of a fluid flow (especially to increase velocity) as it exits (or enters) an enclosed chamber or pipe.

A nozzle is often a pipe or Supersonic jets from bevelled rectangular nozzles book of varying cross sectional area, and it can be used to direct or modify the flow of a fluid (liquid or gas).Nozzles are frequently used to control the rate of flow, speed, direction. A de Laval nozzle (or convergent-divergent nozzle, CD nozzle or con-di nozzle) is a tube that is pinched in the middle, making a carefully balanced, asymmetric hourglass shape.

It is used to accelerate a hot, pressurized gas passing through it to a higher supersonic speed in the axial (thrust) direction, by converting the heat energy of the flow into kinetic energy. Coupling of twin rectangular supersonic jets (X, Z)-plane Z X s Jet 1 h y Jet 2 (Y, Z)–plane Microphone Moveable nozzle Nozzle exit dimensions (mm) Valve 2 Fixed nozzle Air from valve 1 of twin supersonic rectangular nozzle set-up.

detailed depiction of the near acoustic eld of coupled jets is provided in x An. This chapter will elaborate upon the fundamental flow behaviour associated with vortex-rings and jets issuing from nozzles, Part of the Fluid Mechanics and Its Applications book series (FMIA Screech tones of supersonic jets from bevelled rectangular nozzles.

AIAA Journal, 35(7), – CrossRef Google Scholar. Tinney, C. E Cited by: 1. Therefore, the utilization of supersonic rectangular nozzles restrict the working distance as compared to axisymmetric nozzles.

Furthermore, several authors experimentally confirmed the higher spread of the rectangular jets as compared to those with an axial symmetry, in particular for the supersonic ones, Cited by: 8.

The Performance of Supersonic Turbine Nozzles By B. STRATFORD and G.E. SANSOME CoMMuNICATED BY THE DEPUTY CONTROLLER AIRCRAFT (RESEARCH AND DEVELOPMENT), 1VfINISTRY OF AVIATION Reports and Memoranda No.]" June, z Size: 2MB. supersonic jets from various rectangular nozzles []. For instance, in his study regarding the impact of rectangular nozzle aspect ratios on jet noise, Bridges [1] revealed that rectangular nozzles were able to reduce jet noise to a great degree than axisymmetric nozzles.

Rice [2] also investigated theFile Size: 2MB. A supersonic nozzle looks something like this: This type of nozzle is also called as converging-diverging nozzle or de-Laval Nozzle. So, a de-Laval nozzle is designed in such a way that it gives choke to the flow in the throat region and set a max.

For these reasons we would expect to see converging final nozzles on subsonic aircraft like airliners and some fighter jets, while supersonic jets usually have diverging nozzles. If you see a converging nozzle on a supersonic-capable fighter look at it carefully to see if it is articulated for changing shape in flight - which is pretty darn common.

Page 1 Shock Waves in Supersonic Two-Phase Flow of CO 2 in Converging-Diverging Nozzles Masafumi NAKAGAWA1, Menandro Serrano BERANA1, 2, *, Atsushi HARADA1 1Toyohashi University of Technology, Department of Mechanical and Structural System Engineering, Toyohashi City, Aichi, Japan; Tel.: +81 (53)Fax: +81 (53)Email: [email protected]   The present work incorporates the detail study about subsonic and supersonic nozzles.

The concept of method of characteristics is used in designing of nozzle. The program is developed in the language C++, which generates the profile of both the subsonic and supersonic : Dharti Parmar, Meha Setiya, Beena Baloni, S. Channiwala. mixing performance than the rectangular jets in the subsonic and supersonic flow.

n 1, k 2, on 3 conducted the experimental study of supersonic mixer nozzles in a co-flowing stream in the United Technologies Research Centre open jet acoustic wind Size: KB. "Equations are presented for obtaining the wall coordinates of two-dimensional supersonic nozzles.

The equations are based on the application of the method of characteristics to irrotational flow of perfect gases in channels. Curves and tables are included for obtaining the parameters required by the equations for the wall coordinates. A brief discussion of characteristics as applied to nozzle Cited by: 4.

nozzles with conical sections like those used in practical high-speed propulsion applications. LES simulations and experimental measurements in the form of PIV and shadowgraph imaging and far-field acoustic measurement are employed.

The development of the supersonic jets from these nozzles are examined in underexpanded, perfectly expanded and. Even earlier, inwe ran a feature on a Lockheed Martin project for private jets that were designed to fly at supersonic speeds with a very minimal sonic boom.

Understanding subsonic and supersonic nozzle flow using the NAG Library Subsonic and supersonic flow of perfect gas through orifices is a topic which is well studied by a number of researchers. Orial Kryeziu, University College London is currently considering the finite difference method with a.

Supersonic Jet J Active Control of Turbomachine Discrete Fre-quency Noise Utilizing Oscillating Flaps and Pistons J Sound Transmission Through an Aeroelastic Plate into a Cavity J Screech Tones of Supersonic Jets from Bevelled Rectangular Nozzles J Numerically Nonreflecting Boundary and Inter.

This stream then passes through a supersonic nozzle to produce a low supersonic flow entering the MHD accelerator. The MHD accelerator In other words, this high temperature zone downstream of the nozzle exit is responsible for reducing the lean limit of the main chamber mixture by using a supersonic nozzle.

of the nozzle at the test section was to be about inches, so that the half height at the throat was approxi- mately inches. In supersonic nozzle design the conventional two-dimensional nozzle is usually considered to consist of several regions as shown in Fig. These are: File Size: 1MB. Boom says that its supersonic jets will be able to offer round-trip tickets for $5, on routes which would have cost $20, on Concorde in today’s dollars.

A peak frequency formula is also derived from the same model. The noise intensity, directivity, and spectra of supersonic jets from a convergent-divergent nozzle of design Mach number were measured in an anechoic chamber over the Mach number range of to Theoretical results agree very favorably with measurements.

Aeronautics Supersonic Nozzle Design for Low-Noise/High-Thrust at Takeoff Overview. The Supersonics Project within the Fundamental Aeronautics Program at NASA has been investigating nozzle design concepts for commercial supersonic transports entering service around the "N+2" timeframe.

Supersonic jets from bevelled rectangular nozzles [microform] / Edward J. Rice and Ganesh Raman; Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge no Experimental results for a two-dimensional supersonic inlet.

Supersonic gas jets sound like science fiction, but they are actually found throughout our solar system: for example, fast jets of sulfur dioxide stream from the surface of Jupiter's moon Io and.

In this paper critical review of the literature is carried out and a conceptual design of short takeoff supersonic aircraft with cold flow multi-purpose rectangular nozzle has been proposed.

Bachelor of Engineering Final Year Student, Department of Aeronautical Engineering, Kumaraguru College of Technology, Coimbatore –Tamil Nadu. A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology Kareem Akhtar (ABSTRACT) Particle-laden supersonic jets impinging on a at surface are of interest to cold gas-dynamic spray technology.

Solid particles are propelled to a. Supersonic Jets From Conical and Contoured Nozzles Plasma actuators are used to control far-field noise in Mach jets from contoured and conical supersonic axisymmetric nozzles (henceforth, contoured and conical jets, respec-tively).

The contoured nozzle is designed using the method of characteristics for a shock-free jet. It seems that only jet engines with afterburners use adjustable area nozzles (this means adjusting the area of the nozzle but not necessarily the direction).This includes most fighter jets, as well as bombers like the B-1B and Tu Outside of the military or afterburning engines, they don't seem to be used, even for smaller engines.

AIP ADVANCES 6, () The radial dimension of a supersonic jet expansion from conical nozzle Guanglong Chen,1 A. Boldarev,2 Xiaotao Geng,3 Xingjia Li,1 Yunjiu Cao, 1Lili Wang, and Dong Eon Kim3,4,a 1School of Fundamental Studies, Shanghai University of Engineering Science, ShanghaiChina 2Keldysh Institute of Applied Mathematics, Russian Academy of Science, Moscow.

SUPERSONIC NOZZLE DESIGN Paperback – by J.C. CROWN (Author) See all formats and editions Hide other formats and editions. Price New from Used from Paperback, "Please retry" — — $ Paperback from $ Author: J.C.

CROWN. T. Zebbiche and Z. Youbi 92 Emirates Journal for Engineering Research, Vol. 11, No.1, E indice for exit section.

d indice for the length of Kernel. (j) indice for a Segment. j indice for a point. Superscripts * superscript for the value at the throat just afterwards the expansion. K superscript for the iteration. Iso superscript concernig the isovalues curvesFile Size: KB.Enhanced mixing of an axisymmetric jet by aerodynamic excitation [microform] / Ganesh Raman Lewis Research Center ; For sale by the National Technical Information Service Cleveland, Ohio: [Springfield, Va Australian/Harvard Citation.

Raman, Ganesh. & Lewis Research Center.and noise generated by high speed jets issuing from smooth convergent-divergent nozzles as well as facetted nozzles, more typical of military jet aircraft nozzles. The emphasis is on the effects of the grid resolution as well as the methods to reduce the total computation time.

2. Simulation Strategy.

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