Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations-Reference-Cited by-同舟云学术

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Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations

Published:2019-10 Issue: Volume:93 Page:105319
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Löchert Patrick,Huber Kerstin C.,Ghoreyshi Mehdi,Allen Jacob

Funder

Air Force Academy

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

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

2. Ucav Wing Design, Assessment and Comparisons;Nangia,2018

3. Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration;Liersch;CEAS Aeronaut. J.,2016

4. Numerische bewertung innovativer steuerflächen einer generischen lamdaflügel-konfiguration;Winkler,2016

5. Conceptual Design of a 53deg Swept Flying Wing UCAV Configuration;Liersch,2018

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1. Longitudinal Attitude Control and Stability Analysis for a Low Aspect Ratio Flying Wing UAV at High Angle of Attack;International Journal of Aerospace Engineering;2024-01

2. Numerical study of owls' leading-edge serrations;Physics of Fluids;2023-12-01

3. Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle;Journal of Aircraft;2023-11

4. Wing rock mode and its mechanism of a flying-wing aircraft;Flow;2023

5. Trailing-edge jets for UCAV's flight control over a wide speed range;Aerospace Science and Technology;2022-09

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