Tait–Kirchhoff method for determining rotary and unsteady force derivatives-Reference-Cited by-同舟云学术

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Tait–Kirchhoff method for determining rotary and unsteady force derivatives

Published:2014-12 Issue: Volume:39 Page:384-394
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

de Divitiis Nicola^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Analytical Methods Inc., VSAERO User's Manual, Revision E5, April 1994, pp. 1–52.

2. Aerodynamics of Wings and Bodies;Ashley,1985

3. Fuzzy logic-based aerodynamic modeling with continuous differentiability;Chang;Math. Probl. Eng.,2013

4. Wind estimation on a lightweight vertical-takeoff-and-landing uninhabited vehicle;de Divitiis;J. Aircr.,2003

5. Performance and stability analysis of a shrouded-fan UAV;de Divitiis;J. Aircr.,2006

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2. Investigation of pitch damping derivatives for the Standard Dynamic Model at high angles of attack using neural network;Aerospace Science and Technology;2019-09

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