Generation of a reduced-order model of an Unmanned Combat Air Vehicle using indicial response functions-Reference-Cited by-同舟云学术

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Generation of a reduced-order model of an Unmanned Combat Air Vehicle using indicial response functions

Published:2019-12 Issue: Volume:95 Page:105510
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

van Rooij Michel P.C.,Frink Neal T.,Hiller Brett R.,Ghoreyshi Mehdi,Voskuijl Mark

Funder

U.S. Air Force Academy

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Multi-Disciplinary Design and Performance Assessment of Effective, Agile NATO Air Vehicles;Cummings,2018

2. Aerodynamic Design of an Unmanned Combat Air Vehicle in a Collaborative Framework;Van Rooij,2018

3. UCAV Wing Design, Assessment and Comparisons;Nangia,2018

4. Aerodynamic Shaping Design and Vertical Flow Design Aspects of a 53 deg Swept Flying Wing Configuration;Schuette,2018

5. Computation of unsteady transonic flows by indicial methods;Ballhaus;AIAA J.,1978

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4. Introduction to AVT-351: Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles;AIAA SCITECH 2023 Forum;2023-01-19

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