Last edited by Vudozilkree
Friday, July 31, 2020 | History

2 edition of Interaction of a side jet with a supersonic main stream found in the catalog.

Interaction of a side jet with a supersonic main stream

Mark Vladimir Morkovin

Interaction of a side jet with a supersonic main stream

by Mark Vladimir Morkovin

  • 53 Want to read
  • 27 Currently reading

Published by Engineering Research Institute, University of Michigan in [Ann Arbor] .
Written in English

    Subjects:
  • Aerodynamics, Supersonic.

  • Edition Notes

    Statement[by] M. V. Morkovin, C. A. Pierce, Jr. [and] C. E. Craven.
    SeriesEngineering Research Institute. University of Michigan. Engineering research bulletin, no. 35
    Classifications
    LC ClassificationsTL573 .M65
    The Physical Object
    Paginationix, 34 p.
    Number of Pages34
    ID Numbers
    Open LibraryOL6128338M
    LC Control Number52063557
    OCLC/WorldCa6107761

    A supersonic jet stream of water and oxygen gently removes natural skin debris and exfoliates dead skin cells. It oxygenates the tissue & stimulates micro-circulation and lymphatic drainage. Our Jet 3-D peel infuses natural Alpha Hydroxy, Glycolic and Salicylic Acids as well as vitamins and Aloe Vera deep into the skin for a gentle but. @article{osti_, title = {Penetration of a transverse supersonic jet into a subsonic compressible crossflow.}, author = {Erven, Rocky J and Beresh, Steven Jay and Spillers, Russell Wayne and Henfling, John Francis}, abstractNote = {Particle image velocimetry data have been acquired in the far field of the interaction generated by an overexpanded axisymmetric supersonic jet exhausting.

    The jet issuing normally from an orifice into a supersonic stream produces a complex three-dimensional flowfield, sometimes known as jet interaction (JI), which is rich in topological features. Some similarity exists between this flowfield and that induced by a cylindrical protuberance [1,2] that yields a so-called semi-infinite interaction [3].   Parts of North America and Western Europe could experience sonic booms every five minutes if supersonic jets become commercialized, a new study said on Wednesday.

    Richard Branson's Virgin Galactic has announced a partnership with Rolls Royce. The space tourism company will create a new supersonic jet for super-fast travel on Earth. The aircraft will travel. The supersonic jet interaction flow field generated by a sonic circular jet with a pressure ratio of exhausting into a turbulent MACH cross flow over a flat plate was investigated using numerical simulations. The simulations made use of the three-dimensional Reynolds-averaged Navier–Stokes.


Share this book
You might also like
Advanced computer concepts (La Jolla Institute, 1981)

Advanced computer concepts (La Jolla Institute, 1981)

Swimming

Swimming

Industrial utilization of radioisotopes

Industrial utilization of radioisotopes

William Kindley family genealogy: his nine sons and their descendants.

William Kindley family genealogy: his nine sons and their descendants.

Lazy virtues

Lazy virtues

discovery of Canada.

discovery of Canada.

Pembrokes mother.

Pembrokes mother.

Early English literature, to Wiclif.

Early English literature, to Wiclif.

A world of holidays

A world of holidays

Rhythmically Moving

Rhythmically Moving

vita nuova

vita nuova

Annual Earth resources program review.

Annual Earth resources program review.

Financial reconstruction of Austria

Financial reconstruction of Austria

Mt. Rainier National Park-1995 Calendar

Mt. Rainier National Park-1995 Calendar

They were our friends

They were our friends

The mother of Mohammed

The mother of Mohammed

Field Measurement Symposium

Field Measurement Symposium

Interaction of a side jet with a supersonic main stream by Mark Vladimir Morkovin Download PDF EPUB FB2

Get this from a library. Interaction of a side jet with a supersonic main stream. [Mark Vladimir Morkovin]. Interaction of a supersonic stream and a transverse supersonic jet. Two-dimensional jet interaction flowfield predictions with an algebraic turbulence model.

Analysis of the flow-disturbance and side forces due to gaseous secondary injection into a rocket by: Vinson, P.W., J.L. Amick, and H.P. Liepmann: Interaction Effects Produced by Jet Exhausting Laterally Near Base of Ogive–Cylinder Model in Supersonic Main Stream, NASA Memo 12–5–58W, February Google ScholarAuthor: Andrew F.

Charwat. Two-dimensional secondary jet interaction with a supersonic stream. Two-dimensional jet interaction studies at large values of Reynolds and Mach numbers. Frank W. Spaid ; 17 May | AIAA Journal, Vol. 13, No. Experiments on the propagation of mixing and combustion injecting hydrogen transversely into hot supersonic by: The experimentally determined interaction effects of a side jet exhausting near the base of an ogive-cylinder model are presented and discussed.

The interaction force appears to be independent of main-stream Mach number, boundary-layer condition (laminar Author: J. Amick, P. Vinson and H. Liepman. The supersonic jet interaction flow field generated by a sonic circular jet with a pressure ratio of exhausting into a turbulent MACH cross flow over a flat plate was investigated using numerical simulations.

The simulations made use of the three-dimensional Reynolds-averaged Navier–Stokes (RANS) equations coupled with Wilcox’s k-ω turbulence model. Several control jets (CJ) can be used in order to improve the mixing in the initial part of a supersonic jet. This kind of device has been proved to be efficient in subsonic flows.

Supersonic fluid flow and the interaction of strong shock waves to produce jets of material are ubiquitous features of inertial confinement fusion (ICF), astrophysics, and other fields of high energy-density science.

The availability of large laser systems provides an opportunity to investigate such hydrodynamic systems in the laboratory, and to test their modeling by radiation hydrocodes.

Aerospace Science and Technology Interaction Between a Supersonic Hot Jet and a Coaxial Supersonic Flow/ Interaction entre un jet chaud supersonique et un oulement supersonique coaxial [6] Addy A. - Effects of Axisymmetric Sonic Nozzle Geometry on Mach Disc Characteristics, AIAA J., 19, January [7] Clemens N.

T., Mungal M. Transverse injection from a wall orifice is one of the simplest and most promising configurations to enhance the mixing process between the fuel and air in supersonic flows, and it attracts an increasing attention since the early sixties, especially on some scramjet powered vehicles, see Fig.

Fig. 1 represents the computational results obtained by the large eddy simulation. A transverse jet in the supersonic crossflow is one of the most promising injection schemes in scramjet, where the control or enhancement of jet mixing is a critical issue.

In this paper, the effect of the backward facing step on the characteristics of jet mixing was investigated by three-dimensional large eddy simulation (LES). The simulation in the flat plate configuration (step height of 0.

As the liquid jet is injected to a supersonic crossflow from a circular hole, a great number of small droplets with D interaction in the near-nozzle region compared with other regions, which is reflected in the greater proportion of small droplets with D.

First, the use of a "solid body" drag model to describe the jet trajectory is re-examined, extended to include a supersonic main stream, and modified to alleviate the most untenable of the.

Both primary and secondary fluids were air at the same stagnation temperature, but the secondary stagnation pressure was varied from about to 2 times the primary value; injection was sonic and the jet issued into the primary stream through a slit of constant width at 0 deg, 8 deg, 23 deg, and 50 deg upstream (the angle being measured from.

A group of scientists at NASA‘s Ames Research Center in Mountain View, Calif. has successfully captured the first images showing interactions of supersonic jet shockwaves. The technique used to record them has been in development for over 10 years.

NASA says this breakthrough will greatly contribute to its Aeronautics Research Mission Directorate. Jet streams are fast flowing, narrow, meandering air currents in the atmospheres of some planets, including Earth. On Earth, the main jet streams are located near the altitude of the tropopause and are westerly winds (flowing west to east).

Their paths typically have a meandering shape. Jet streams may start, stop, split into two or more parts, combine into one stream, or flow in various. Interaction between a supersonic airstream and a sonic jet injected through a diamond-shaped orifice. Mixing of a Hydrogen Jet from a Wedge Shaped Injector into a Supersonic Cross Flow.

Optimization of the Fuel Injector for the Supersonic Combustor Using a. Why can't jet engines operate with supersonic air. "Because there has been no business case to develop an engine with supersonic flow at entry to the compressor." The advantages would be the same that led to todays transonic (supersonic relative flow over part of the blade span) compressors, ie smaller and lighter.

A rocket engine uses a nozzle to accelerate hot exhaust to produce thrust as described by Newton's third law of motion. The amount of thrust produced by the engine depends on the mass flow rate through the engine, the exit velocity of the flow, and the pressure at the exit of the engine.

The value of these three flow variables are all determined by the rocket nozzle design. It centers on supersonic jets that can fly faster than the speed of sound, or miles per hour.

Indeed, while most commercial airliners today fly at between and miles per hour [ ]. Brown, A. M.,“Characterization of Side Load Phenomena Using Measurement of Fluid/Structure Interaction,” 38th Joint Propulsion Conference and Exhibit, AIAA Paper No.

Pekkari, L.-O.,“Aeroelastic Stability of Supersonic Nozzles With Separated Flow,” 29th Joint Propulsion Conference and Exhibit, AIAA Paper No. Dubbed the AS2, the supersonic private jet would comfortably fit 12 passengers while achieving a cruising speed of Mach by way of its three .Supersonic Flow Jet x y z Figure 1: Schematic representation of the general flow field developing due to the side jet interaction.

If KF exceeds 1, there is a gain additionally to the thrust of the jet itself resulting from the interaction of the side jet with the flow, if it is smaller than 1, the jet thrust is alleviated.