National Aeronautics and Space Administration www.nasa.gov 1 The Beginner’s Guide to Wind Tunnels with TunnelSim and TunnelSys Tom Benson Inlets and Nozzles.

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The Beginner’s Guide to Wind Tunnels with TunnelSim and TunnelSys
Presentation transcript:

National Aeronautics and Space Administration 1 The Beginner’s Guide to Wind Tunnels with TunnelSim and TunnelSys Tom Benson Inlets and Nozzles Branch NASA Glenn Research Center Carol Galica Educational Programs Office NASA Glenn Research Center Anthony Vila Mechanical Engineering Student Vanderbilt University 4 Jan 10

National Aeronautics and Space Administration 2 OUTLINE Background / Rationale Beginner’s Guide to Wind Tunnels (BGT) TunnelSim TunnelSys Summary

National Aeronautics and Space Administration 3 BACKGROUND For the past 12 years, NASA Glenn has been building a web-based textbook, the Beginner’s Guide to Aeronautics, (BGA) that includes information about airplanes, turbine engines, model rockets, kites, baseball, compressible aerodynamics and hypersonic aerodynamics. The textbook includes scientific and mathematical descriptive pages, interactive Java applets, teacher created activities, podcasts, and PowerPoint presentations.

National Aeronautics and Space Administration 4 Sample Web Pages Beginner’s Guide To Aeronautics FoilSim software Pages

National Aeronautics and Space Administration 5 The Beginner’s Guide to Wind Tunnels (BGT) Create a new section of the BGA dealing with Wind Tunnels Wind Tunnel Testing (Web version of Pope’s Wind Tunnel Testing) Gather existing web-based information Develop new web pages and interactive software

National Aeronautics and Space Administration 6 BGT Index - Part 1

National Aeronautics and Space Administration 7 Typical Web Pages Low Speed Tunnel Strain Gage

National Aeronautics and Space Administration 8 BGT Index - Part 2

National Aeronautics and Space Administration 9

National Aeronautics and Space Administration 10 TunnelSim – Software to Design a Tunnel A Java applet that solves the one-dimensional continuity equation through an open tube. Flow assumed to be incompressible and inviscid. Student can vary geometry or flow conditions at the bellmouth, test section, or diffuser, and the program computes conditions at all other places through the tunnel Output includes variation through the tunnel and conditions in the test section Violations of assumptions are flagged. On-line user’s manual and BGT support for science and math.

National Aeronautics and Space Administration 11 TunnelSim

National Aeronautics and Space Administration 12 TunnelSys – Software for Design Class Three Java applications dealing with three aspects of wind tunnel testing: Design of Wind Tunnel Model Wind Tunnel Testing Techniques Data Post-Processing Programs pass information to each other by data files Suggest a fourth team member to act as program manager Based on FoilSim – determine lift performance of a wing desig n On-line user’s manual and demonstration applets

National Aeronautics and Space Administration 13 TunnelSys – Design Program

National Aeronautics and Space Administration 14 TunnelSys – Test Program

National Aeronautics and Space Administration 15 TunnelSys – Processing Program

National Aeronautics and Space Administration 16 Future Plans Later versions of TunnelSim to include closed circuit tunnels, loss estimates in the corners, and power requirements for the motor Later versions of TunnelSys to include drag estimation, and lift calculation based on user static pressure number and location. Additional web pages and topics to be added based on user feedback on current configuration.

National Aeronautics and Space Administration 17 SUMMARY A new section of the BGA has been developed which deals with the subject of wind tunnels and wind tunnel testing techniques. Site became active in September, Access by entering “Beginner’s Guide to Wind Tunnel” in your search engine. Two major Java programs have been developed; TunnelSim for the design and analysis of a low speed wind tunnel, and TunnelSys for use in a design class dealing with model design, testing, and post-processing Later versions of software and web pages to be determined by user feedback and NASA support.

National Aeronautics and Space Administration 18 This work was supported by Tony Springer Aeronautics Research Mission Directorate (ARMD) NASA Headquarters and NASA Glenn Educational Programs Office

National Aeronautics and Space Administration 19 QUESTIONS ?