Problem 3.15: The landing weight of the Concorde, a supersonic transport, is approximately 245,000lb. The planform has a curved, swept leading edge and is referred to as an ogee; however, assume that it can be approximated as a delta wing having an aspect ratio of 1.7. The wing span is 25.5m. If the airplane lands at a speed that is 20% above the stalling speed, what is the landing speed when landing at SSL conditions? Note: Use Fig. 3.78 to estimate missing parameters.