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Technical Article A4

Shockwave Formation and Sonic Booms

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Shock wave formation:

Let us picture an aircraft taking off from the airstrip. As the aircraft moves, it pushes air molecules out of its way, continuously creating waves of compressed and uncompressed air. These air pressure waves move away from the aircraft in all directions at the speed of sound just like the ripples one can see by dropping a pebble in a pond.

Fig. TA-A4-1 

As the aircraft's speed becomes faster than the speed of sound, (approximately 760 miles per hour or about 1,225 km per hour, at sea level at 57 degrees F), the air pressure waves begin to pile up ahead of the aircraft and compress, forming shock waves. A similar phenomenon is that of a 'bow wave' that accumulates at the front of a boat as it moves through water. These shock waves start at the nose, wingtips and other forward-projecting parts of the aircraft and form a cone trailing back from the plane and expanding up, down, and out to the sides. When this cone spreads across the ground, it creates a sonic boom around the width of the cone's base due to the release of the shock wave during a very short time interval.

A point to be noted at this stage is that a sonic boom does not only happen the instant an aircraft surpasses the speed of sound. Sonic booms are observed when any aircraft, which is traveling faster than the speed of sound, passes overhead. It is not a sign that the aircraft just overcame the sound barrier, but rather a sign that the aircraft is traveling faster than sound. It is also to be noted that a sonic boom is heard only after the aircraft passes. This is because if the plane is flying at less than the speed of sound, the sound of the plane travels ahead of the plane. Thus, people on the ground can hear the plane coming toward them. However, the sound of a plane flying faster than the speed of sound cannot be heard on the ground until the aircraft has passed.

All aircraft generate two cones, one at the nose and the other at the tail.  They are usually of similar strength and the time interval between the two as they reach the ground is primarily dependent on the size of the aircraft and its altitude. Most people on the ground cannot distinguish between the two and they are usually heard as a single sonic boom. Sonic booms created by vehicles the size and mass as the space shuttles are very distinguishable and two distinct booms are easily heard.

Mach numbers:

Mach numbers are used to describe the speed of planes flying near or above the speed of sound. A Mach number is found by dividing the speed of an airplane by the speed of sound at the plane's altitude. For example, the Mach number of a plane flying at 1,520 mph at sea level would be 2.  Modern airliners cruise at an altitude of about 35,000 feet (9,000 meters) and a speed of about Mach 0.80 to Mach 0.85. Flight that is slightly faster or slower than Mach 1 is known as transonic flight. A plane that is significantly slower than Mach 1 is subsonic whereas a plane that is significantly faster than Mach 1 is supersonic, and that which is at or faster than about Mach 5 is hypersonic.

Impact on human beings:

The noise levels of sonic booms are varied. Sonic booms are measured in pounds per square foot of overpressure. Overpressure is the amount of increase over normal atmospheric pressure that surrounds us. Here are a few parameters to judge the level of sonic booms according to the level of damage they can inflict.

At one pound of overpressure, which is produced by supersonic aircraft flying at normal operating altitudes, there will be no damage to structures. At an overpressure between 1.5 - 2 pounds it would be annoying to the people living in the vicinity of where it occurs. When there is an overpressure of 2 - 5 pounds rare minor damage could occur. From this point onwards, the likelihood of structural damage increases. Tests however reveal that sound structures have been undamaged even by pressures up to 11 pounds. Sonic booms produced by aircraft flying supersonic at altitudes of less than 100 ft, creating between 20 and 144 pounds of overpressure, have been experienced by humans without injury.  There could be damage to the ears when overpressures reach 720 pounds.  Lung damage will occur when there are overpressures of 2160 pounds.

Factors influencing sonic boom:

The main reason that we hear a sonic boom is because of the shock waves generated by the aircraft when it crosses the speed of sound. However there are several other factors that can influence sonic booms - weight, size and shape of an aircraft, the altitude and flight path at which the aircraft is flying and the outside temperature and pressure.

A larger and correspondingly heavier aircraft displaces more air and creates more lift to sustain flight thereby generating stronger shock waves. It will therefore create sonic booms stronger and louder than those of smaller and lighter aircraft.

The altitude of an aircraft determines the distance shock waves travel before reaching the ground. This is a significant factor on the intensity of the shock wave. As the shock cone gets wider, and it moves outward and downward, its strength gets diminished. Accordingly, the higher the aircraft, the greater the distance the shock wave has to travel, reducing the intensity and audibility of the sonic boom.  Among the factors influencing sonic booms, an increase in altitude is the most effective method for reducing the intensity of sonic boom.  

The width of the cone beneath the aircraft is approximately one mile for each 1000 feet of altitude. For example, an aircraft flying supersonic at 50,000 feet can produce a sonic boom cone about 50 miles wide. The sonic boom, however, will not be uniform. Maximum intensity is directly beneath the aircraft, and decreases as the lateral distance from the flight path increases until it ceases to exist because the shock waves refract away from the ground. The lateral spreading of the sonic boom depends only upon altitude, speed, and the atmosphere - and is independent of the aircraft's shape, size and weight.

The ratio of aircraft length to maximum cross sectional area also influences the intensity of the sonic boom. The longer and more slender the aircraft, the weaker would be the shock waves. The shorter and stockier the vehicle, the stronger would be the shock waves. Increasing speeds above Mach 1.3 results in only small changes in shock wave strength. The direction of travel and strength of shock waves are influenced by wind, speed, and direction, and by air temperature and pressure. At speeds slightly greater than Mach 1, their effect can be significant, but their influence is small at speeds greater than Mach 1.3. Distortions in the shape of the sonic booms can also be influenced by local air turbulence near the ground. This, too, will cause variations in the overpressure levels.

Sonic boom lines:

Aircraft maneuvering can cause distortions in shock wave patterns. Some maneuvers pushovers, acceleration, and 'S' turns - can amplify the intensity of the shock wave. Hills, valleys, and other terrain features can create multiple reflections of the shock waves and affect intensity.

On maps and globes of the earth, the locations of the equator, the Arctic and Antarctic circles, and the tropics of Cancer and Capricorn are clearly marked.  These circles indicate certain characteristics of the apparent journey that the sun makes over the earth's surface each year. There are two other conjured circles on the earth's surface that few people know about. They are called "sonic boom lines," and they indicate the latitudes where the earth's surface velocity is equal to the speed of sound.

The rotation of the earth causes many parts of the surface to spin at velocities that exceed the speed of sound. Since the circumference of the earth is roughly 24,000 miles, the surface speed at the equator due to the rotation of the earth is about 1,000 miles per hour (well above the speed of sound). Using simple trigonometry, it is easy to compute the latitude where the earth's surface is moving at precisely the speed of sound. At sea level and zero degrees Celsius that latitude is 44 degrees 21 minutes, and a circle drawn around the earth at that latitude is a sonic boom line. There are two such lines; one in the Northern Hemisphere and the other in the Southern Hemisphere. Unlike the equator and tropics, the exact locations of the sonic boom lines vary according to local altitude and air temperature. Although these effects are very small, they are enough to make the exact locations of the boom lines laborious to determine and in continuous flux. That is why cartographers refuse to put these lines on their maps.

Technically, the sonic boom lines are the intersections of an imaginary cylinder with the earth's surface. The center line of the cylinder is aligned with the earth's rotational axis and the surface of the cylinder (which represents all points that are rotating at the speed of sound) pierces the earth's surface at the two sonic boom latitudes. The two supersonic atmospheric regions that are directly above the sonic boom lines at the earth's surface are called, the 'nether regions'. These small areas of the atmosphere dissipate the sonic boom shock waves into outer space, thus preventing the shock waves from causing a continuous, annoying boom to the people on the surface. The earth's motion around the sun and the sun's motion through the cosmos do not affect the sonic boom phenomenon nor produce one of their own. This is because sound waves cannot travel through the vacuum of outer space.

Though sonic booms are not often heard these days in most inhabited parts of the world it is a field that required wide study in order to enable engineers to design aircrafts that would cause the minimum sonic boom and thereby minimum discomfort and damage to people.

Additional documents on sonic booms

bullet In addition other documents may be available on the download page under the Sonic Boom heading.

Sonic Disturbance Associated With the Reentry Breakup of STS-107

Area of disturbance:

Fig. TA-A4-2 

The fact that the residents of Nacogdoches heard the sonic boom so pronounced does not mean that the shuttle went through the sound barrier to subsonic speed at that time, but only that the cone representing the sonic boom intersected the ground in that area.  This analysis needs to be fine tuned by questioning more residents to determine the area of the sonic disturbance with greater degree of certainty and estimating the exact size and shape of the cone.

This information by itself is probably not enough to establish the altitude of the shuttle as it was breaking up.  However, it may help to test other data and analysis for their accuracy.

Diagram of Sonic Boom Footprint

The sonic booms heard by witnesses to the breakup of X-15A-3 were very similar to those heard by the residents of Nacogdoches when the Columbia broke up in a similar manner.

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