Supersonic Transport Aircraft Design

The extended nose of a supersonic aircraft helps to shape the forward shock wave, ensuring smooth airflow and efficient aerodynamics.

Canard surfaces are small wings located on the nose of the aircraft, these surfaces are fixed for the QueSST and provide nose-up trim specifically at the low boom design point.

The wing of the QueSST is designed to protect the intake of the engine from shockwaves, this ensures a smooth flow of air into the engine for efficient operation.

Single piece wing skins are used on the QueSST, which enhances structural integrity and efficiency in stress distribution.

The mini T-tail on the QueSST design is an important feature responsible for minimizing the impact of shockwaves, minimizing the sonic boom and improving overall noise reduction.

The speed of an object that exceeds the speed of sound, approximately 768 mph (1,236 km/h).

The loud, intense sound produced when an aircraft breaks the sound barrier. It occurs due to the buildup of pressure waves in front of the aircraft.

A type of aircraft designed to fly at supersonic speeds without producing a significant sonic boom. This is achieved through specific design features.

The world's first supersonic passenger jet, known for its distinctive delta-shaped wings. Its loud sonic boom restricted its flight routes.

The ability of the X-59 aircraft to fly at supersonic speeds without generating a significant sonic boom. This is achieved through its unique design and engineering features.

The removal of the forward-facing cockpit window on the X-59 aircraft to reduce noise and improve aerodynamic efficiency. The pilot relies on cameras for visibility.

Placing the X-59's engine on top of the fuselage instead of below it, directing the noise away from the ground and minimizing the sound heard by people on the ground.