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This reference provides an overview of the aerothermodynamics and CFD updates, including the coefficient of drag variation with angle of attack and Mach. The text language is English.
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Jayme Zott1-31-08AerothermodynamicsCoefficient of DragCFD updateref. on all CFD – Brian Budzinski, Chris Strauss AAE 450 Spring 2008
Cd varies with AOA and M Matlab code: Inputs: Mach, Altitude, AOA Outputs: Cd (potentially drag) solve_cd.m Based on historical and empirical (wind tunnel) data Note: does not take exhaust plume into consideration Overview Ref. [1] Sutton, Biblarz Ref. [2] Toft Ref [3] Vanguard AAE 450 Spring 2008 Aerothermodynamics
CFD Updates • Mesh Completed • Solver running • Continuity residuals are too high Future Work Ref. [4] Budzinski, Strauss • Correct CFD for Vanguard check • Begin running scaled/new configurations AAE 450 Spring 2008 Aerothermodynamics
References • Sutton, George P., and Oscar Biblarz. Rocket Propulsion Elements. New York: John Wiley & Sons, Inc., 2001. 2. Toft, Hans Olaf. “Aerolab” Software. [http://users.cybercity.dk/~dko7904/software.htm. accessed 1/30/08] 3. The Martin Company, “The Vanguard Satellite Launching Vehicle”, Engineering Report No. 11022, April 1960 4. Budzinski, Brian, and Strauss Christopher. 5. AAE 450 Senior Design Class: Spring 2006, “Project Infinity Final Report”, April 2006. 6. Fluent: Fluid Flow Modeling Webinars, Compressible Flows - Solving Compressible Flow Problems; June 25, 2005. [http://www.fluent.com/elearning/resources/webinars/webinars_cfd.htm . accessed 1/29/08] 7. Numerous ME/AAE professors and graduate students: Tsohas, Merkle, Blaisdell, Ni AAE 450 Spring 2008
Backup slides Ref. [2] Toft Ref [3] Vanguard Ref. [1] Sutton, Biblarz AAE 450 Spring 2008
Backup slides Ref. [2] Toft Ref [3] Vanguard Ref. [2] Toft Ref [4] Strauss AAE 450 Spring 2008
Backup Slides Ref. [1] Sutton, Biblarz AAE 450 Spring 2008
Backup slides AAE 450 Spring 2008