Aerospace Research and Development Group, LLC
Numeriqs introduces Legal Description Reader for AutoCAD, a metes and bounds parsing tool built to convert legal text into structured boundary geometry inside AutoCAD. The software reads bearings, distances, curves, and alias references, transforming written descriptions into drawable line and arc segments with full visibility into closure and computation. Legal… Continue reading The post Numeriq…
We’re proud to announce the launch of Numeriqs, our new software brand, focused on precision computational tools for CAD and engineering professionals. Numeriqs began with a simple idea — to make advanced analytical methods accessible in practical, field-ready software. It serves technical professionals who value reliability, clarity, and control. Our… Continue reading The post Introducing Numeri…
Do no harm Make things better Respect others Be fair and just in dealings with others Show kindness toward others — Dr. Bruce Weinstein Continue reading The post Five Tenants of Engineering Ethics appeared first on Aerospace Research and Development Group, LLC .
As a Professional Engineer, I dedicate my professional knowledge and skill to the advancement and betterment of human welfare. I pledge: To give the utmost of performance; To participate in none but honest enterprise; To live and work according to the laws of man and the highest standards of professional… Continue reading The post The Engineer’s Creed appeared first on Aerospace Research and Deve…
I have spent an inordinately long period of time resolving the intricacies in combustor diffuser. Considering the lower temperatures we are dealing with, pressure losses can be rather devastating. As a result, I looked at a myriad of texts and methods to develop our pressure model for our combustion system.… Continue reading The post Diffuser Frustration appeared first on Aerospace Research and D…
The low pressure (LP) fan and high pressure (HP) compressor are designed in a similar manner. These both suffer from design problems that are exacerbated by low hub/tip (h/t) ratio blades. One such problem is blade twist. We wanted to compare four vortex theory models, including Mixed-Vortex swirl distribution and three… Continue reading The post Swirl Distribution in Low Hub/Tip Ratio Blades app…
The axial flow turbofan HP compressor and turbine were, and continue to be, a battle between size, efficiency, and power. These two components affect the overall performance of the engine. While the design is still an on-going challenge, I can see the fun parts coming. Materials and elegantly designed component… Continue reading The post HP Compressor and Turbine Update appeared first on Aerospa…
I have been involved in a small footprint turbofan for a few years now. While the overall parameters of each engine section are understood, the intricacies of achieving each requirement are mind-boggling. Currently Aerospace Research and Development Group, LLC (AeroRND) is neck deep in the annular combustor design challenges (burner… Continue reading The post Turbofan Research – Combustor Design …
I have studied turbofan theory and design for over 3 years straight. My pet project, a small footprint turbofan, came with me to Aerospace Research and Development Group, LLC. (AeroRND). The project has taken on new dimensions and has grown a life of its own (like Frankenstein, only the Mel… Continue reading The post Small Footprint Turbofan Research appeared first on Aerospace Research and Deve…
While I’ve enjoyed every position with every company I’ve worked with, not every position fulfills me in ways that I want. In some cases, I missed the ability to design. In other cases, I missed the ability to strategically move the company. As a small business owner, I get to… Continue reading The post My Story – Why a Small Business Startup appeared first on Aerospace Research and Developmen…
