How to Calculate Shock Wave Cone Angle and Plane Speed in a Sonic Boom Situation

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SUMMARY

The discussion focuses on calculating the shock wave cone angle and the speed of a plane in a sonic boom scenario. The plane is flying at an altitude of 1.4 km and has traveled 2.4 km horizontally when the sonic boom is heard. The correct angle of the shock wave cone is determined using the sine function, yielding an angle of approximately 35.7 degrees. The speed of the plane is calculated using the relationship between the speed of sound (343 m/s) and the plane's speed, resulting in a Mach number of 1.78, although this was initially miscalculated by some participants.

PREREQUISITES
  • Understanding of trigonometric functions, specifically sine and tangent.
  • Familiarity with the concept of Mach number and its calculation.
  • Knowledge of basic physics principles related to sound and motion.
  • Ability to apply Pythagorean theorem in right-angled triangles.
NEXT STEPS
  • Study the derivation of the Mach number and its significance in aerodynamics.
  • Learn how to apply trigonometric functions in real-world physics problems.
  • Explore the concept of shock waves and their implications in supersonic flight.
  • Practice solving problems involving right-angled triangles and Pythagorean theorem applications.
USEFUL FOR

Students in physics or engineering fields, educators teaching aerodynamics, and anyone interested in the dynamics of supersonic flight and sonic booms.

negatifzeo
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Homework Statement


You look directly overhead and see a plane exactly 1.4·km above the ground, flying faster than the speed of sound. By the time you hear the sonic boom, the plane has traveled a horizontal distance of 2.4·km.

(a) Find the angle of the shock wave cone.

(b) Find the speed of the plane (Mach number).


Homework Equations


Sin (shock wave cone angle)=(c/v)

PLane Speed= v/c

v=velocity of source

c=speed of sound

The Attempt at a Solution


The plane is 1400 meters high. When the shockwave is heard, the plane has traveled 2400 meters horizontally. Sound travels at 343 m/s. 1400/343 gives me 4.08 seconds. 2400/4.08 gives the plane a speed of 588 m/s.

Sin-1(343/588)=35.7 degrees. Of course, I'm here because these are not the correct answers and I don't know why. Any clues as to what I did wrong would be greatly appreciated.
 
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Hi negatifzeo! :smile:

You're not thinking clearly. :frown:

The sound leaves the plane before it's overhead.

Draw a diagram. There's a right-angled triangle in it. You know one of the angles has sin c/v (which one?). Then use Pythagoras' theorem! :smile:
 
I don't understand. It makes sense that the planr makes a sound before its directly overhead, of course. But how can you solve for sin c/v without knowing the aircraft's speed?
 
negatifzeo said:
But how can you solve for sin c/v without knowing the aircraft's speed?

Because v is an unknown, just like x in ordinary algebra equations.

Draw the diagram … use v, or a multiple of v, where you would normally use a number … and you'll get an equation in v (maybe linear, maybe quadratic) … which you can then solve.

Try it (and start with the diagram)! :smile:
 
I'm having problems with this question too.

I understand that the angle is Tan-1 (1.4/2.4) = 30.25 degrees

But how do you go about finding the mach number? I also calculated the speed as 588 m/s, making the Mach speed 1.78, but that wasn't right.
 

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