High Angle of Attack Parameter Estimation of Cascaded Fins Using Neural Network-Reference-Cited by-同舟云学术

High Angle of Attack Parameter Estimation of Cascaded Fins Using Neural Network

Published:2013-01 Issue:1 Volume:50 Page:272-291
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sinha Manoranjan¹,Kuttieri Rajesh Ayilliath¹,Ghosh Ajoy Kanti²,Misra Ajay³

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721302, India

2. Department of Aerospace Engineering, Indian Institute of Technology, Kanpur 208016, India

3. DIAT, Defense Institute of Advanced Technology, Pune 411025, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031912

Reference17 articles.

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2. JonesR. T. “Operational Treatment of the Non-uniform Lift Theory in Airplane Dynamics,” NACA TN-667, 1938.

3. TobakM. “On the Use of the Indicial Function Concept in the Analysis of Unsteady Motions of Wings and Wing-Tail Combinations,” NACA Rept. 1188, 1954.

4. TobakM.SchiffL. B. “On the Formulation of the Aerodynamic Characteristics in Aircraft Dynamics,” NASA TR-R-456, 1976.

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