Click on "Play Entire ZEUS Training Video" below to view the
entire training or on the links below to view indivdual sections.
Displayed Run Times In: (hours:minutes:seconds)
| Play Entire ZEUS Training Video |  |
(11:22:47) |
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)