This paper describes the results of an ongoing research project to develop a solution to aircraft loss of control caused by an unreliable airspeed indication by incorporating the concept of an aircraft digital twin.Omar Hazbon AlvarezLuis B. Gutierrez Zea...
Overall, the N-1M, with its elevons and wing-tip drag rudders, performed creditably well and proved the possibility of the flying wing concept. However, the engines hidden in the airfoil suffered from overheating while the drooped wing tips used for stability were found to be unnecessary [...
Reduce risks, shorten aircraft development time and effectively tackle design complexities using a digital twin and Agile systems engineering. Learn more.
The Digital Twin (DT) concept emerged many years ago in 1991 when it was mentioned for the first time in the publication of David Gelernter [1] and was taken up some years later by Professor Michael Grieves in 2002 during his university course. The term was introduced by NASA in their pr...
2.TheDigitalTwinConcept Considerthefollowinghypotheticalcapability.In2025,the United States Air Force (USAF) takes delivery of the first of a new model of aircraft, tail number 25-0001. Along with the physical aircraft, the USAF also receives an as- ...
Gain early insights into the integrated aircraft behavior, from the concept phase onwards. Effectively re-use your models throughout your design cycle. Get a preview of the trial scenarios. This trial utilizes Simcenter 3D, Simcenter Amesim and ...
The new generation segment is anticipated to exhibit the fastest CAGR over the forecast period. The concept ofdigital twinsis gaining momentum in the MRO landscape for new generation aircraft. A digital twin is a virtual representation of an aircraft that simulates its performance and maintenance ne...
In past years, the concept of the Digital Twin has spread across all industrial sectors. Using advanced machine learning and artificial intelligence for analyzing data collected by sensors and/or historical data, Digital Twins serve as a digital counterpa...
Although the concept of active blade flapping has been shown to enhance the performance of a conventional rotor, the main challenges to this approach are the mechanical complexity of the rotor hub, the inertial forces due to active blade-flapping, and the additional power required by the blade-...
A hybrid wing body (HWB) concept twin aisle passenger was designed, and wing-mounted liquid hydrogen-fueled turbo-generators with 30 MW in a full turbo-electric HEP architecture. 14 EM-driven propellers on a DP concept are located on the trailing edge, a BLI configuration. These distributed ...