Shock diamond

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Shock diamonds are the bright areas seen in the exhaust of this statically mounted Pratt & Whitney J58 engine on full afterburner, burning off the last of the SR-71 fuel before the program ended. J58 AfterburnerT.jpeg
Shock diamonds are the bright areas seen in the exhaust of this statically mounted Pratt & Whitney J58 engine on full afterburner, burning off the last of the SR-71 fuel before the program ended.

Shock diamonds (also known as Mach diamonds or thrust diamonds) are a formation of standing wave patterns that appear in the supersonic exhaust plume of an aerospace propulsion system, such as a supersonic jet engine, rocket, ramjet, or scramjet, when it is operated in an atmosphere. The "diamonds" are actually a complex flow field made visible by abrupt changes in local density and pressure as the exhaust passes through a series of standing shock waves and expansion fans. The physicist Ernst Mach was the first to describe a strong shock normal to the direction of fluid flow, the presence of which causes the diamond pattern. [1] :48

Contents

Mechanism

Shock diamonds behind a Lockheed SR-71 Blackbird. SR-71 Blackbird afterburn.jpg
Shock diamonds behind a Lockheed SR-71 Blackbird.
Shock diamonds from an F-16 taking off with afterburner South Carolina F-16 taking off in Afghanistan.jpg
Shock diamonds from an F-16 taking off with afterburner
Aerojet Rocketdyne RS-25 engine test at NASA's Stennis Space Center Shuttle Main Engine Test Firing.jpg
Aerojet Rocketdyne RS-25 engine test at NASA's Stennis Space Center
An F-22 Raptor with shock diamonds behind it Lockheed Martin F-22A Raptor JSOH.jpg
An F-22 Raptor with shock diamonds behind it
USAF F-22 Raptor flying in knife edge during a high-speed low-altitude pass over Airventure in full afterburner with Mach diamonds at sunset F22afterburneratAirventure.jpg
USAF F-22 Raptor flying in knife edge during a high-speed low-altitude pass over Airventure in full afterburner with Mach diamonds at sunset

Shock diamonds form when the supersonic exhaust from a propelling nozzle is slightly over-expanded, meaning that the static pressure of the gases exiting the nozzle is less than the ambient air pressure. The higher ambient pressure compresses the flow, and since the resulting pressure increase in the exhaust gas stream is adiabatic, a reduction in velocity causes its static temperature to be substantially increased. [2] The exhaust is generally over-expanded at low altitudes, where air pressure is higher.

As the flow exits the nozzle, ambient air pressure will compress the flow. [2] The external compression is caused by oblique shock waves inclined at an angle to the flow. The compressed flow is alternately expanded by Prandtl-Meyer expansion fans, and each "diamond" is formed by the pairing of an oblique shock with an expansion fan. When the compressed flow becomes parallel to the center line, a shock wave perpendicular to the flow forms, called a normal shock wave or Mach disk. This locates the first shock diamond, and the space between it and the nozzle is called the "zone of silence". [3] The distance from the nozzle to the first shock diamond can be approximated by

where x is the distance, D0 is the nozzle diameter, P0 is flow pressure, and P1 is atmospheric pressure. [3]

As the exhaust passes through the normal shock wave, its temperature increases, igniting excess fuel and causing the glow that makes the shock diamonds visible. [2] The illuminated regions either appear as disks or diamonds, giving them their name.

Eventually the flow expands enough so that its pressure is again below ambient, at which point the expansion fan reflects from the contact discontinuity (the outer edge of the flow). The reflected waves, called the compression fan, cause the flow to compress. [2] If the compression fan is strong enough, another oblique shock wave will form, creating a second Mach disk and shock diamond. The pattern of disks and diamonds would repeat indefinitely if the gases were ideal and frictionless; [2] however, turbulent shear at the contact discontinuity causes the wave pattern to dissipate with distance. [4]

Diamond patterns can similarly form when a nozzle is under-expanded (exit pressure higher than ambient), in lower atmospheric pressure at higher altitudes. In this case, the expansion fan is first to form, followed by the oblique shock. [2]

Alternative sources

Shock diamonds beneath Masten Space Systems Xoie rocket during the Lunar Lander Challenge competition-winning landing. Kluft-photo-MSS-Xoie-LLC-L2-landing-Img 1282.jpg
Shock diamonds beneath Masten Space Systems Xoie rocket during the Lunar Lander Challenge competition-winning landing.

Shock diamonds are most commonly associated with jet and rocket propulsion, but they can form in other systems.

Natural gas pipeline blowdowns

Shock diamonds can be seen[ by whom? ] during gas pipeline blowdowns because the gas is under high pressure and exits the blowdown valve at extreme speeds.[ citation needed ]

Artillery

When artillery pieces are fired, gas exits the cannon muzzle at supersonic speeds and produces a series of shock diamonds. The diamonds cause a bright muzzle flash which can expose the location of gun emplacements to the enemy. It was found that when the ratio between the flow pressure and atmospheric pressure is close, which can be achieved with a flash suppressor, the shock diamonds were greatly minimized. Adding a muzzle brake to the end of the muzzle balances the pressures and prevents shock diamonds. [1] :41

Radio jets

Some radio jets, powerful jets of plasma that emanate from quasars and radio galaxies, are observed to have regularly-spaced knots of enhanced radio emissions. [1] :68 The jets travel at supersonic speed through a thin "atmosphere" of gas in space, [1] :51 so it is hypothesized that these knots are shock diamonds.[ citation needed ]

See also

Related Research Articles

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<span class="mw-page-title-main">Ramjet</span> Supersonic atmospheric jet engine

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<span class="mw-page-title-main">Shock wave</span> Propagating disturbance

In physics, a shock wave, or shock, is a type of propagating disturbance that moves faster than the local speed of sound in the medium. Like an ordinary wave, a shock wave carries energy and can propagate through a medium but is characterized by an abrupt, nearly discontinuous, change in pressure, temperature, and density of the medium.

<span class="mw-page-title-main">Turbojet</span> Airbreathing jet engine which is typically used in aircraft

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Compressible flow is the branch of fluid mechanics that deals with flows having significant changes in fluid density. While all flows are compressible, flows are usually treated as being incompressible when the Mach number is smaller than 0.3. The study of compressible flow is relevant to high-speed aircraft, jet engines, rocket motors, high-speed entry into a planetary atmosphere, gas pipelines, commercial applications such as abrasive blasting, and many other fields.

<span class="mw-page-title-main">Nozzle</span> Device used to direct the flow of a fluid

A nozzle is a device designed to control the direction or characteristics of a fluid flow as it exits an enclosed chamber or pipe.

<span class="mw-page-title-main">Mach wave</span> Pressure wave

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de Laval nozzle Pinched tube generating supersonic flow

A de Laval nozzle is a tube which is pinched in the middle, making a carefully balanced, asymmetric hourglass shape. It is used to accelerate a compressible fluid to supersonic speeds in the axial (thrust) direction, by converting the thermal energy of the flow into kinetic energy. De Laval nozzles are widely used in some types of steam turbines and rocket engine nozzles. It also sees use in supersonic jet engines.

<span class="mw-page-title-main">Afterburner</span> Adds additional thrust to an engine at the cost of increased fuel consumption

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<span class="mw-page-title-main">Rocket engine nozzle</span> Type of propelling nozzle

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<span class="mw-page-title-main">High pressure jet</span>

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References

  1. 1 2 3 4 Michael L. Norman; Karl-Heinz A. Winkler (July 1985). "Supersonic Jets". Los Alamos Science . 12: 38–71.
  2. 1 2 3 4 5 6 Scott, Jeff (17 April 2005). "Shock Diamonds and Mach Disks". Aerospaceweb.org. Retrieved 6 November 2011.
  3. 1 2 Niessen, Wilfried M. A. (1999). Liquid chromatography-mass spectrometry. Vol. 79. CRC Press. p. 84. ISBN   978-0-8247-1936-4.
  4. "Exhaust Gases' Diamond Pattern". Florida International University. 12 March 2004. Archived from the original on 7 December 2011. Retrieved 6 November 2011.