transonic
Actually, transonic speed is not a speed faster than that of sound. Transonic speed is approx. Equal to the speed of sound, not faster.
Faster than the speed of sound.
Transonic speed occurs when an object is traveling at a speed that is close to the speed of sound, typically between 0.8 and 1.2 times the speed of sound. At transonic speeds, airflow around the object can become turbulent, leading to changes in aerodynamic forces and potential control issues.
When an airplane slows from the speed of sound, it goes through a region called the transonic zone. During this process, shock waves and changes in air pressure occur, which can lead to turbulence and potential loss of control if not managed properly. Pilots need to carefully control the aircraft's speed to safely transition through the transonic zone.
Transonic speeds are when an object is moving near the speed of sound, experiencing a mix of subsonic and supersonic airflow. Subsonic speeds are when an object is moving at speeds below the speed of sound. At transonic speeds, airflow can become unpredictable, leading to effects like shock waves and buffeting.
Mach 0.8-1.0
Depending on the aircraft it ranges from 160 knots to 130 knots
Edwin J. Saltzman has written: 'In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)' -- subject(s): X-29 aircraft, Wave drag, Lift, Airfoil profiles, Swept forward wings, Drag, Transonic speed
I. Frank Sakata has written: 'Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft' -- subject(s): Aerodynamics, Transonic, Supersonic planes, Transonic Aerodynamics
The cruising speed of a Cessna aircraft can vary depending on the model, but generally ranges from 100 to 200 knots (115 to 230 mph).
As pilots get closer to the speed of sound, the air resistance they experience increases significantly. This can lead to an effect known as "transonic buffeting" where the airflow over the aircraft becomes turbulent. Pilots must carefully control their speed and altitude to manage these effects and prevent loss of control of the aircraft.
The stall speed of the Airbus A340-200 typically ranges from about 105 to 115 knots, depending on factors such as aircraft weight, configuration, and environmental conditions. Stall speed is the minimum speed at which an aircraft can maintain level flight and varies based on these variables. For precise values, refer to the aircraft's specific operating manual or performance data.