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A shock wave is a type of propagating disturbance. When a wave moves faster than the speed of sound in a liquid, gas or plasma (a "fluid", in physics terminology) it is a shock wave. Like an ordinary wave, a shock wave carries energy, and can propagate through a medium. It is characterized by an ...

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Reason for trailing edge boudary layer separation at transonic speed on subsonic airfoil

Prior to the shock stall, the shock induced boundary layer separation can be classified mainly into 2 types illustrated in Fig 1 (I couldn't get better resolution). Model A illustrates a bubble ...
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What is the importance of Mach number (M) on shock waves?

My primary question is: what is the importance of Mach number (M) on shock waves? Although I believe confirming and/or answering the below will help clarify my misconceptions. When a wave moves ...
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Do ramjets use variable geometry supersonic inlets?

Ramjets are very often portrayed as super simple, I've read on few occasions that the only moving parts in a ramjet are the fuel pumps. However, turbojets operating at similiar speeds (mach 2 - mach 3)...
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Knowing the shape of a shock wave, and the relative speed of object making it: can the density of medium be calculated? [closed]

This is somehow an Astrophysics question, as images exist of star core remnants of an explosion travelling very fast in a supposed empty space, leaving a conical shock wave behind, the doubt is about ...
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Transonic buffet - reason for a rapid movements of the shockwave along the wing chord line?

I know that transonic aerodynamic buffet is caused by the separated turbulent boundary layer striking the airframe (horizontal stabilizer, wings, fuselage) with considerable force causing a high ...
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How is it possible for supersonic aircraft to push air out of the way?

If the force (pressure) can be transferred/propagated only at the speed of sound, how are supersonic aircraft able to move air out of their way/do work on the air? It seems that they must transfer the ...
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What is primary cause of shock induced separation (shock stall)?

In the video link above describing Prandtl Meyer Waves, lecturer stated (at 22:40) a very important fact on which he based his first half of the lecture. "Mach wave (mach lines) deflect the flow ...
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How can one approximately guesstimate wave drag?

Wave drag is an especially high drag that affects supersonic vehicles above mach 1, but I've found it hard to find source materials to estimate wave drag. I'm looking at the transonic region till Mach ...
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“Fundamental of Aerodynamics” 5th editon, example about oblique shock. Is the author's solution wrong?

I am reading "Fundamentals of Aerodynamics" 5th edition, J.D.Anderson. If you have the book, go to chapter 9: Oblique shock and expansion waves. Please look at example 9.2, page 618: Consider a ...
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How does the V22 Osprey manage such high rotor speeds without shock waves?

I read somewhere that the engineers presented an ingenious solution to the rotor tip shockwave problem, except the article didn't actually explicitly mention it. So, does anybody actually know if ...
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What are the effects of shockwaves on normal and supersonic aircraft?

What are the effects on the speed of the plane, does it effects the body of the plane, and do shockwaves cause major damage to the plane. I know that flying at Mach 1 is really risky, but what's the ...
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What is the difference between a shock wave and an expansion wave?

Studying high speed aerodynamics I have found a question asking for what happens to static temperature for an airflow passing through an expansion wave. The correct answer states that it decreases- ...
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What happens to the pressure and density of air passing through shock waves?

I understand that the pressure and density of air increase as the air gets closer to shock waves and the pressure and density of air that has escaped the shock waves increase as well. Then, what ...
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Can a transonic airfoil have two shock waves?

I am currently running CFD cases on a transonic airfoil at Mach 0.75 and performing an angle-of-attack sweep to evaluate its performance. When I reached the angle of attack of 4.5 degrees (which I ...
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What would the density profile of this shock wave look like, roughly?

The YouTube video titled Shock Wave Formation in Transonic Flight shows a hand-held video of a visible shock wave extending from the top of a jet engine near the front. The shock wave is visible by ...
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Can a supersonic plane use a subsonic wing if the nosecone shock produces subsonic airflow around the wing?

A supersonic plane will produce shock waves off the nose cone, as seen below: These oblique shocks reduce the speed of the air that the wing experiences. If the plane is at a low enough Mach number, ...
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Why is the flow ahead of a shock wave chaotic?

Here is the image of a shock wave on a cone in a small supersonic wind tunnel, the white lines are the condensations formed in the test chamber due to flow expansion. Why are the condensations so ...
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What do the components of a shockwave's visual artefacts represent?

On a recent flight, I was able to observe visual artefacts over the wing (Boeing 767-300 in cruise). You can see them in the image below; they look like creases in a surface. They moved forwards and ...
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Why does this shockwave not touch the body that creates it?

In the shock wave of the next image (in a blunt body) Why the wavefront is in front of the object? It does not assume that if the object travels faster than the speed of sound wave front should be ...
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Can a flow which is initially supersonic, become subsonic without a shock wave?

I am doing my college project in which air is first accelerated to supersonic conditions in a nozzle. Then it is added into slow moving subsonic air. I see that my flow becomes supersonic and then ...
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Reason behind formation of Mach rings [duplicate]

At night, some jet aircraft like Mirage 2000 leave a trail of discs behind in their jet, these are also known as Mach rings or Mach diamonds. How are they formed and what atmospheric conditions ...
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How does a wing mounted jet engine on a supersonic airplane prevent the interference in the flow due to Shock? [duplicate]

Wing mounted jet engines face the free stream at Mach number 1 or above, and they work perfectly for Mach numbers below 1 as well, even though the free stream characteristics change a lot after Mach 1....