Flight Dynamics of the Boomerang, Part Two: Effects of Initial Condition and Geometrical Configuration
Author:
Affiliation:
1. Tokai University, Hiratsuka 259-1292, Japan
2. University of Tokyo, Kawasaki 212-0021, Japan
3. Nihon University, Funabashi 274-8501, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11158
Reference1 articles.
1. Flight Dynamics of the Boomerang, Part 1: Fundamental Analysis
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