DARcorporation Announces Reseller Agreement | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Recent Daily Episodes

Episode Date

Airborne Unlimited-
Monday

Airborne Unmanned-
Alt. Wednesdays

Airborne Flight Training-Alt. Wednesdays

Airborne Unlimited-
Friday

Airborne Special Programs!
Airborne-YouTube  Airborne Unlimited--08.03.20 Airborne-Unmanned--08.05.20   NEW! Airborne-Flight Training--07.29.20 Airborne Unlimited--08.07.20  The 2020 Avionics Innovation Preview!

Airborne On ANN

Airborne Unlimited--08.03.20

Airborne-Unmanned--08.05.20

NEW! Airborne-Flight Training--07.29.20

Airborne Unlimited--08.07.20

Airborne's Annual April 1st Episode

Sun, Jul 30, 2017

DARcorporation Announces Reseller Agreement

Research In Flight Will Carry FlightStream Aerodynamics Software

Design, Analysis and Research Corporation (DARcorporation), announces the addition of a software program into its lineup of airplane design software products.

FlightStream, developed by Research in Flight, will be sold and supported by DARcorporation. FlightStream will be demonstrated at EAA AirVenture in Oshkosh.

FlightStream is a high fidelity aerodynamics tool perfectly suited for the aircraft designers. Users can easily surface mesh their CAD models with the integrated meshing tool. The unique vorticity based flow solver, which uses only a surface mesh, produces accurate solutions in a fraction of the time required by full volume mesh CFD solvers. The FlightStream solver can model aircraft, propellers, high-lift devices and jet engine effects. The intuitive user interface, utility of the meshing tool and robustness of the flow solver allow users of all skill levels to obtain accurate aerodynamic results quickly and easily.

What sets FlightStream apart from similar software is its accuracy. To ensure accuracy and reliability, extensive validation has been performed using peer reviewed wind tunnel data. Comparing FlightStream results with experimental data for all types of configurations and flight conditions has successfully validated its solutions.

"Research in Flight is excited to join forces with DARcorporation in bringing to market a new paradigm in numerical aerodynamics." - Roy Hartfield, Co-Founder, Research in Flight.

“We started our own development of a high-speed accurate CFD tool, but when we evaluated FlightStream we knew this is the tool to use for fast aerodynamic analysis and design. The next logical step was to become a reseller.” – Willem Anemaat, President, DARcorporation

(Source: DARcorporation news release. Image provided)

FMI: www.darcorp.com/Software/FlightStream

Advertisement

More News

Small UAV Coalition Voices Support for the Unmanned Delivery Services Act

Legislation Would Further The Ongoing Dialogue Between Industry And Government The Small UAV Coalition sent a letter, this week, to House Communications and Technology Subcommittee>[...]

US Delivers Humanitarian Aid to Beirut by C-17

11 Pallets Of Humanitarian Aid, Which Contained More Than 28,800 Military Field Rations In a joint endeavor to assist the Lebanese Armed Forces and the people of Lebanon after a de>[...]

US Advanced Aerobatic Team Training Underway

14th FAI World Advanced Aerobatic Championships Will Take Place 15-24 Of July 2021 This past week, two of the eight Advanced Aerobatic Team pilots came to Union City, Tennessee (KU>[...]

ANN's Daily Aero-Term (08.08.20): Aircraft Approach Category

Aircraft Approach Category A grouping of aircraft based on a speed of 1.3 times the stall speed in the landing configuration at maximum gross landing weight. An aircraft must fit i>[...]

ANN FAQ: Follow Us On Instagram!

Get The Latest in Aviation News NOW on Instagram Are you on Instagram yet? It's been around for a few years, quietly picking up traction mostly thanks to everybody's new obsession >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2020 Web Development & Design by Pauli Systems, LC