Catalog excerpts
J2 DEVELOPERENHANCE VALUE FROM EXISTING DATA With J2 software there’s no need to discard the data models you already use to calculate aerodynamics, mass, inertia and thrust characteristics. J2 Developer and the Software Development Kit (SDK) enable you to integrate old and new to find the perfect solution and optimise return on investment. What’s more, you get all the configuration, version control, data management capability, integrated visualisation, and comprehensive analyses functionality of the J2 Universal Tool-Kit on your existing data models. 1. Re-Use Existing Solutions • No need to extract data out of working solutions. Simply plug them into the J2 Universal Tool-Kit • Perform sensitivity studies using the existing pre-compiled solution as a baseline; superimpose variations on top 2. Open Interface • Models written in any language can be wrapped using the Software Development Kit provided • Templates written for most languages 3. User-orientated Services • No need to calculate derivatives to find dynamic effects • Local angle of attack is automatically calculated, enabling lift distribution to be calculated based on platform, dihedral and twist • Velocity changes shown on each strip, illustrating changes due to Roll, Yaw and Pitch For further information contact J2 Aircraft Dynamics on +44 (845) 052 9489 AIRCRAFT DYNAMICS or email: sales@j2aircraft.com Predicting Performance
Open the catalog to page 1Advantages and Benefits Easy to Use Graphical Interface Compatible with any units Re-Use Output Ports Visualize your Data Evaluate Tolerances Standard Open Interface Windows Libraries are connected straight into aircraft Models using a simple GUI to connect input and output signals. This means there is no time wasted creating text files for mapping Unit conversions are no longer a headache. This is easily managed through the GUI which handles all data conversions Once the system has been connected, the output signals become model parameters. They can then be used anywhere in the model for...
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