In business since 1993, Avionics Systems, LLC is the leading builder of custom instrument panels for Experimental Aircraft - it's all we do! With years of experience inLancair, RV, Velocity, Seawind, Carbon Cub, Kitfox, and many others, including one-off and custom projects, we have the ...
XPanel 5000 is the most feature rich, easiest to use, economical, aircraft instrument panel design software available.buy now *Current draw will be calculated using numbers provided by the user. **When operating in "Trial Mode" users cannot save or export panels. ...
A device has been constructed to monitor automatically the magnitude and polarity of electrostatic fields associated with an aircraft in flight. It is small,self-contained apart from an ancillary photographic recorder,and operates from the aircraft 400Hz supply. Logarithmic amplifier techniques are used...
Experimental and numerical investigations of unsteady aerodynamic derivatives for transport aircraft configurations. In order to improve the accuracy of the experimental and numerical methods used for the prediction of the dynamic derivatives, systematic investigations have been performed using the new lightwei...
Aerotronics has the technical expertise to address your aircraft needs. Our staff of technicians and pilots are with you from your initial choice of a homebuilt thru your first flight and beyond.
Multilayered sandwich like struc- tures can be used in aircraft structures and other applica- tions, such as robot arms for effective vibration control. Much of the literature is related to one of the attributes (high strength/weight or increased energy absorption) as mentioned above. Also, ...
InstrumentModelSensitivityMeasure range Hammer PCB 86E80 23.11 mV/N 222.0 N (peak) Accelerometer KISTLER 3.86 mV/g 10 Hz–25 kHz Data Acquisition LMS SCR05 – – The EM plate geometric parameters and material properties are summarized in Table 3. The material properties, i.e.,...
Summarizing the existing research results, it can be seen that due to the structural and mechanical characteristics, the influence of wind-driven rain on the additional aerodynamic force of the main beam is different from those of aircraft thin wings, building windward surfaces, and cable structures...
Experimental and Numerical Study of the Influence of Pre-Existing Impact Damage on the Low-Velocity Impact Response of CFRP Panels. Materials 2023, 16, 914. [Google Scholar] [CrossRef] Zhang, Y.; Yan, S.; Wang, X.; Guan, Y.; Du, C.; Fan, T.; Li, H.; Zhai, J. An ...
Specially designed one piece molded cabin and fuselage including firewall, seats, instrument panel and floor. Airframe built from 4130 chrome moly aircraft tubing. Cockpit, and all structural panels are built from Carbon fiber; the same materials used in a Formula One Race Car. Easy fabrication...