At the 18 km cruising altitude of Concorde, a passenger aircraft that flew at twice the speed of sound, the temperature was -57∘C. What was the Concorde's cruising speed?
At the 18 km cruising altitude of Concorde, a passenger aircraft that flew at twice the...
27 Concorde in Flight Constants The Concorde was a supersonic aircraft used for trans-Atlantic travel in the 1980s and 1990s, having a length of 61.8 m when sitting on the ground on a typical day when the temperature is 16.0 °C. The Concorde is primarily made of aluminum. In flight at twice the speed of sound, friction with the air warms the Concorde's skin and causes the aircraft to lengthen by 30.0 cm. (The passenger cabin is on rollers, so...
The supersonic aircraft Concorde has a length of 61.8 m when sitting on the ground on a typical day when the temperature is 13.0 ∘C . The Concorde is primarily made of aluminum. In flight at twice the speed of sound, friction with the air warms the Concorde's skin and causes the aircraft to lengthen by 22.0 cm . (The passenger cabin is on rollers, so the airplane expands around the passenger cabin.) Take the coefficient of linear expansion for...
The supersonic aircraft Concorde has a length of 62.0 m when sitting on the ground on a typical day when the temperature is 18.0 ℃. The Concorde is primarily made of aluminum. In flight at twice the speed of sound, friction with the air warms the Concorde's skin and causes the aircraft to lengthen by29.0 cm. (The passenger cabin is on rollers, so the airplane expands around the passenger cabin.)Take the coefficient of linear expansion for aluminum to be α = 2.40×10−5 ℃.What...
concorde concorde supersonic transport flew at mach 2.2 at 20km altitude. concorde had four engines, each of which produces a thrust of 170kN. it mass on take -off was 185 tons and fuel was consumed at a rate of 22.6tons/h a) what is the Mach angle? b) How far behind the aircraft was it heard in the ground(take the atmosphere to have constant sound speed equal to 340m/s)? c) what was the ratio of lift to drag 2hours into flight?
C | | Search Course Home KHW 1 - Ch 17 ± Concorde in Flight Review Constants l Periodic Table Part A The Concorde was a supersonic aircraft used for trans-Atlantic travel in the 1980s and 1990s, having a length of 61.7 m when sitting on the ground on a typical day when the temperature is 18.0 °C. The Concorde is primarily made of aluminum. In flight at twice the speed of sound, friction with the air warms the Concorde's...
Concorde The Concorde supersonic transport flew at M = 2.2 at 20 km altitude. Air is decelerated isentropically by the engine inlet system to a local Mach number of 1.3. The air passed through a normal shock and was decelerated further to M = 0.4 at the engine compressor section. Assume, as a first approximation, that this subsonic diffusion process was isentropic and use standard atmosphere data for freestream conditions. -Determine the temperature, pressure and stagnation pressure of the air...
A General Aviation aircraft is cruising at an altitude of 15,000 ft. A research payload brings in 1500 lbm/min of external air at 190 mph without changing the density, pressure, or temperature of the air compared to standard conditions. This air is then moved through a duct where the outlet is 200 in2, where it encounters a metric thermal sensor. Determine the expected temperature of the air at the sensor in degrees Celsius
A military jet cruising at an altitude of 12.0 km and speed of 2400. km/h burns fuel at the rate of 38.9 L/min. How would you calculate the amount of fuel the jet consumes on a 1600. km mission? Set the math up. But don't do any of it. Just leave your answer as a math expression. Also, be sure your answer includes all the correct unit symbols. fuel consumed = 1 x o ?
Question 2 10 pts What is the atmospheric pressure at a cruising altitude of 10 km? Use the scale height of H-7.4 km and the pressure at the sea level is 1013 hPa. Answer in hPa to three significant digits.
At an altitude of 11,000 m (a typical cruising altitude for a jet airliner), the air temperature is -52.5 ∘C and the air density is 0.356 kg/m3. The molar mass of air is 28.8 g/mol. What is the pressure of the atmosphere at that altitude? (Note: The temperature at this altitude is not the same as at the surface of the earth, so the equation P=P0exp(−MgyRT) doesn't apply.)