Stability and Control of Tailless Aircraft Using Variable-Fidelity Aerodynamic Analysis
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
2. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034052
Reference31 articles.
1. CummingsR. M.SchutteA. “An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161,” AIAA Paper 2010-4392, June 2010.
2. RoyJ. L.MorgandS. “SACCON CFD Static and Dynamic Derivatives Using elsA,” AIAA Paper 2010-4562, June 2010.
3. Strategy for Dynamic CFD Simulations on SACCON Configuration
4. Computational Study of Static And Dynamic Vortical Flow over the Delta Wing SACCON Configuration Using the FOI Flow Solver Edge
5. Overview of Stability and Control Estimation Methods from NATO STO Task Group AVT-201
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