Rapid Prediction of Hybrid Wing Body Aerodynamics-Reference-Cited by-同舟云学术

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Rapid Prediction of Hybrid Wing Body Aerodynamics

Published:2022-06-20 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2022 Forum
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Author:

DiMaggio Griffin A.¹,Hartfield Roy J.¹,Ahuja Vivek²

Affiliation:

1. Auburn University

2. Research in Flight

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3298

Reference14 articles.

1. Okonkwo, P. "Conceptual Design Methodology for Blended Wing Body Aircraft," PhD Dissertation,Cranfield university, 2016.

2. Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration

Cited by 5 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. Validation of a Mid-Fidelity Approach for Aircraft Stability and Control Characterization;AIAA AVIATION 2023 Forum;2023-06-08

2. Experimental validation of a Surface Vorticity flow solver for swept wings;AIAA AVIATION 2023 Forum;2023-06-08

3. Application of a Semi-Empirical Method to Model Subsonic Vortex Lift over Sharp Leading-Edge Delta Wings;AIAA SCITECH 2023 Forum;2023-01-19

4. Hybrid Wing Body Pitch Control with a Surface-Vorticity Solver;AIAA SCITECH 2023 Forum;2023-01-19

5. Pressure Distributions for Bodies of Revolution in Compressible Flows Using an Advanced Panel Method;AIAA SCITECH 2023 Forum;2023-01-19

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