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FB16 Maschinenbau · Offered in SoSe 2026
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Inhalt: Kompressible Stromfadentheorie, allgemeiner Verdichtungsstoß, Prandtl-Meyer-Expansion, gasdynamische Grundgleichung, kompressible Profiltheorie, kompressible Tragflügeltheorie, kompressible Grenzschichten. Lernziele:Die Studierenden können das Strömungsfeld um Profile, Tragflügel und Rümpfe für kompressible Strömungsverhältnisse berechnen, Aufgaben mit Stoß-Expansionstheorie lösen, den Einfluss der Grenzschicht berücksichtigen und sie kennen das Charakteristikenverfahren für komplexere Geometrien. DATE TOPIC Do, 27. Apr. 23 Introduction and thermodynamics fundamentals, speed of sound Do, 4. Mai 23 Laval Nozzle flow (quasi 1D, compressible isentropic flow) Do, 11. Mai 23 Supersonic wind tunnels, normal and oblique shock theory Do, 25. Mai 23 Shock reflection, application to engine inlet ducts Do, 1. Jun. 23 Prandtl-Meyer expansion (at sharp edges and curved surfaces), Do, 15. Jun. 23 Compressibility corrections (Goethert rule, Prandtl-Glauert rule), Do, 15. Jun. 23 sonic barrier, critical pressure coefficient, supercritical aerfoils Do, 22. Jun. 23 Sub- and supersonic profiles, linearised supersonic flow theory, forces on an aerfoil, buffetting Do, 29. Jun. 23 Compressibility corrections 3D (Prandtl-Glauert-Goethert rule), Three-dimensional compressibility effects for wings, yawed wings in supersonic flow Do, 6. Jul. 23 Summary and trial exercise
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