1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research-Reference-Cited by-同舟云学术

1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Gross Andreas¹,Pearman Cory¹,Kremer Rodney¹,Napier Brandon¹,Gosla Calvin¹,Kurz Armin¹,Mack Steffen¹,Brehm Christoph¹,Heine Benjamin¹,Radi Alexander¹,Marovic Boris¹,Retzko Stefan¹,Feindler Nico¹,Zickler Bettina¹,Fasel Hermann¹,Osbrink Andrew²

Affiliation:

1. University of Arizona

2. Advanced Ceramics Research, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6416

Reference15 articles.

1. 2Foster, J., Cunningham, K., Fremaux, C., Shah, G., Stewart, E., Wilborn, J., and Gato, W. "Dynamics Modeling and SimulationofLarge Transport Airplanes inUpset Conditions," AIAApaper AIAA-2005-5933,Aug. 2005

2. AirSTAR: A UAV Platform for Flight Dynamics and Control System Testing

3. 5Murch, A., and Foster, J. "Recent NASA Research on Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes," AIAApaper AIAA-2007-463, Jan.2007

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Using approximate similitude to design dynamic similar models;Aerospace Science and Technology;2019-11

2. Active Control of Laminar Separation: Simulations, Wind Tunnel, and Free-Flight Experiments;Aerospace;2018-10-30

3. Low-Cost High-Endurance Solar-Powered Unmanned Aerial Vehicle;35th AIAA Applied Aerodynamics Conference;2017-06-02

4. Hybrid Turbulence Model Simulations of Partially Stalled Airfoil Flow;AIAA Journal;2016-04

5. Numerical and Experimental Wind Tunnel and Flight Testing of Active Flow Control for Modified NACA 643-618 Airfoil;53rd AIAA Aerospace Sciences Meeting;2015-01-03