Did you know…
Why does the sound barrier exist?
Short answer
The sound barrier exists because pressure disturbances travel through air at the speed of sound. Below Mach 1 the air ahead of an aircraft receives warning and flows smoothly around it; near Mach 1 that warning can no longer arrive, so air compresses abruptly into shock waves. Those waves cause a steep drag rise and control changes that early aircraft could not overcome.

Sound is the messenger
Air is not a solid wall in front of an aircraft; it moves aside because the pressure disturbance from the approaching nose reaches it first and starts it moving. That disturbance travels at exactly the speed of sound, since a sound wave and a pressure signal are the same thing. As long as the aircraft is slower than sound, the signal runs ahead, the air begins to divert before the aircraft arrives, and the flow bends smoothly around wings and fuselage. As the aircraft speeds up, the signal has less of a head start. At the speed of sound it has none: the aircraft arrives at the same instant as its own pressure wave, and the air has no warning at all.
Shock waves and the drag rise
Air that cannot move aside in advance is compressed almost instantly in a very thin layer, a shock wave, across which pressure, density and temperature jump. Creating that jump takes energy that comes from the aircraft, and it appears as a sudden increase in drag, often several times the subsonic value in the transonic range around Mach 0.8 to 1.2. Shocks form first over the wing's curved upper surface, where air is accelerated to local supersonic speed while the aircraft itself is still subsonic. Behind the shock the airflow tends to separate from the surface, producing heavy buffet and a loss of lift. The barrier is therefore not at one exact speed; it is a band of speeds in which the behaviour of the air changes character.
Why it felt like a wall
The name dates from the Second World War, when fast propeller fighters in steep dives reached about Mach 0.8 and met effects nobody had designed for. Shocks over the wing moved the centre of lift rearward, pitching the nose down further into the dive, a tendency called Mach tuck. Hinged elevators sitting in the disturbed air behind a shock lost their authority, so pulling on the stick did nothing, and several aircraft broke up or flew into the ground. Propellers made it worse, because their tips went supersonic before the aircraft did and lost thrust. Engineers knew the physics of bullets and artillery shells, which pass through the region routinely, but it took jet and rocket engines, thin wings and an all-moving tail to give a piloted aircraft the thrust and control to do the same. Once those tools existed, the barrier remained real as a drag rise and a sonic boom, but ceased to be a limit.
More questions

Physics of flight
Why can't a Corsair pilot apply full power when going around after a failed carrier landing?
Because at low speed and high power the Corsair would drop its left wing suddenly and with almost no warning, due to propeller torque. If the throttle was… more…

Physics of flight
What did the phrase "banking with intent to turn" mean among F-104 pilots?
It was a joke among Canadian F-104 pilots: banking the aircraft "with intent to turn" referred to its poor low-speed turning. Its sustained turn capability… more…

Julian Herzog (Website) (CC BY), vía commons Physics of flight
What is "flight envelope protection," which the A320 pioneered?
A set of limits embedded in the flight control software: it calculates the flight envelope, adds a safety margin, and blocks pilot inputs that would take the… more…

Julian Herzog (Website) (CC BY), vía commons Physics of flight
What is the A320's SHARP package for?
SHARP (SHort AiRfield Package) improves takeoff and landing performance on short runways and is designed to increase low-speed lift. It combines aerodynamic… more…

Physics of flight
What flaw sank Vought's all-metal V-141 fighter?
It wasn't a single flaw: tests showed the V-141 still flew poorly, was prone to spinning, and also suffered tail flutter, which is why it was rejected. It… more…

Physics of flight
What wind tunnel did NACA use to study the Corsair, and how big was it?
The full-scale 30- by 60-Foot Tunnel at the Langley Research Center, in Hampton, Virginia. NACA dedicated the facility on 27 May 1931 and used it to test the… more…