A Psychoacoustic Feature Extraction and Spatio-Temporal Analysis Framework for Continuous Aircraft Noise Monitoring. [PDF]
He T, Hou J, Chen D.
europepmc +1 more source
Image processing-based warning system for preventing the fuel selector valve from remaining closed in small trainer aircraft. [PDF]
Çoban İH, Kazan FA.
europepmc +1 more source
The design of an airfoil for a high-altitude, long-endurance remotely piloted vehicle [PDF]
Airfoil design efforts are studied. The importance of integrating airfoil and aircraft designs was demonstrated. Realistic airfoil data was provided to aid future high altitude, long endurance aircraft preliminary design.
Maughmer, Mark D., Somers, Dan M.
core +1 more source
AI based decision-making system for tooling design of aircraft product assembly with developed knowledge retrieval algorithm. [PDF]
Miah MH +7 more
europepmc +1 more source
Two-stage scheduling optimization model for taxiways on the basis of time slot derivation. [PDF]
Tang J, Zhang Q, Lian G, Wen T.
europepmc +1 more source
Vision-Based Vehicle State and Behavior Analysis for Aircraft Stand Safety. [PDF]
Tang K +5 more
europepmc +1 more source
Aircraft Conceptual Structural Design Using the AMMIT Structural Analysis Tool [PDF]
Aircraft conceptual structural design is the process of developing and refining an idea for an aircraft into a feasible structural design. The process typically involves multiple evaluations of a single configuration and can require designers to examine ...
Horvath, Bryce L.
core +1 more source
Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft [PDF]
Assessed are the risks associated with the lift/cruise fan technology V/STOL aircraft program. Three candidate concepts for the technology aircraft design approach are considered: the lowspeed only modification, the full performance modification, and the
core +1 more source
A new type of aircraft icing detection system. [PDF]
Renno NO +12 more
europepmc +1 more source
Preliminary candidate advanced avionics system for general aviation [PDF]
An integrated avionics system design was carried out to the level which indicates subsystem function, and the methods of overall system integration. Sufficient detail was included to allow identification of possible system component technologies, and to ...
Birkhead, L. M. +3 more
core +1 more source

