Skip to main content
Download PDF
- Main
Numerical and Analytical Investigation of the Unsteady Lift Characteristics of Plunging-Pitching-Flapping Wings
- Muoio, Ryan
- Advisor(s): Taha, Haithem E
Abstract
Three methods for computing the unsteady lift response due to basic kinematic motion---plunging, pitching, and flapping---are compared. The first two methods are analytical models developed by Theodorsen and Leishman, while the third method is a numerical method known as the unsteady vortex lattice method. The MATLAB code for this numerical method is included. All calculations are evaluated for the potential flow case.
Main Content
For improved accessibility of PDF content, download the file to your device.
Enter the password to open this PDF file:
File name:
-
File size:
-
Title:
-
Author:
-
Subject:
-
Keywords:
-
Creation Date:
-
Modification Date:
-
Creator:
-
PDF Producer:
-
PDF Version:
-
Page Count:
-
Page Size:
-
Fast Web View:
-
Preparing document for printing…
0%