ZEUS Training Videos

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Table Of Contents


1.0  ZEUS Overview (00:39:50)

2.0  ZEUS Input Data Structure (00:37:54)

3.0  Formulation of the Full Euler Solver with Boundary Layer Option (00:20:21)

4.0  Linearized Euler Solver for Rapid Frequency-Domain Aeroelastic Analysis (00:14:26)

5.0  Input Bulk Data Cards for the Euler Solver (00:26:11)

6.0  Automated Mesh Generation (00:51:55)

7.0  Input Cards for Aerodynamic Modeling (01:53:06)

8.0  Aerodynamic Modeling Guidelines (00:30:01)

9.0  Miscellaneous Input (00:22:12)

10.0  Spline (00:42:00)

11.0  Flutter Analysis (00:41:02)

11.1   Sample Case: AGARD 445.6 Wing (00:19:51)

12.0  STABDRV Module for Generating Aerodynamic Stability and Damping Derivatives (00:09:58)

13.0  Maneuver Loads (MLOADS) Analysis (00:24:10)

13.1   Sample Case:AGARD 445.6 Wing (00:08:26)

14.0  Gust Loads (GLOADS) Analysis (00:08:31)

14.1   Sample Case: Forward-Swept Wing with Canard Configuration (00:04:45)

15.0  Static Aeroelastic / Trim Analysis (00:50:35)

15.1   Theoretical Background (00:16:08)
15.2   Static Aeroelastic Analysis: Trim & Bulk Data Card Input (00:12:28)
15.3   Sample Case for Trim Analysis (00:21:57)

16.0   Examples for Complex Configurations (01:56:25)

16.1   Subsonic, Transonic & Supersonic Aerodynamics Of L56a18 Wing-body-tail Configuration (00:22:35)
16.2   Steady Hypersonic Analysisof Bent-Nose (00:25:15)
16.3   Steady and Unsteady Cp of F-5 with Tip Tank and Underwing Store (00:17:13)
16.4   Frequency-Domain Flutter Analysis of a Twin-Engine Transport Flutter Model (00:24:50)
16.5   Boeing Joined-Wing Trim Analysis (00:26:19)