Search results
Results from the WOW.Com Content Network
The X-48C featuring two engines and inboard vertical stabilizers Wind tunnel testing on a 12 feet (3.7 m) wide blended wing body model was completed in September 2005. [ 14 ] [ 15 ] During April and May 2006, NASA performed wind tunnel tests on X-48B Ship 1 at a facility shared by Langley and Old Dominion University .
An aeroplane can stall at any speed, so monitoring the ASI alone will not prevent a stall. The critical angle of attack (AOA) determines when an aircraft will stall. For a particular configuration, it is a constant independent of weight, bank angle, temperature, density altitude , and the center of gravity of an aircraft .
English: The X-48C Hybrid Wing Body aircraft flies over Rogers Dry Lake on Feb. 28, 2013, from NASA's Dryden Flight Research Center, Edwards Calif. The long boom protruding from between the tails is part of the aircraft's parachute-deployment flight termination system.
EFIS on an Airbus A380 EFIS on an Eclipse 500 Garmin G1000 on a Diamond DA42 Primary flight display of a Boeing 747-400. In aviation, an electronic flight instrument system (EFIS) is a flight instrument display system in an aircraft cockpit that displays flight data electronically rather than electromechanically.
The plane would later achieve a speed of just over 2,000 miles per hour, nearly 50% faster than Concorde. “The overall design of the XB-70 was a thing of beauty,” says Tony Landis, a historian ...
An air data boom provides air pressure, temperature, and airflow direction data to data acquisition systems for the computation of air, ground, and water vehicle orientation, speed, altitude/depth, and related information. Air data booms can be used as primary sensors or as a "measurement standard" of which primary sensors and instruments are ...
AN/SPS 48e on board the USS Ronald Reagan (CVN-76).. The AN/SPS-48 is a US naval electronically scanned array, air search three-dimensional radar system manufactured by ITT Exelis and deployed in the 1960s as the primary air search sensor for anti-aircraft warships.
Focusing schlieren systems can use compact optics with a large background illumination pattern, which is particularly easy to produce with a projection system. For systems with large demagnification, the illumination pattern needs to be around twice larger than the field of view to allow defocusing of the background pattern. [5] [6]