Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability-Reference-Cited by-同舟云学术

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Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability

Published:2019-06 Issue: Volume:89 Page:1-10
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Voß A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Conceptual design and aerodynamic analyses of a generic UCAV configuration;Liersch,2014

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

3. Multidisciplinary conceptual design of a UCAV configuration;Krüger,2011

4. Design and sizing of a parametric structural model for a UCAV configuration for loads and aeroelastic analysis;Voß;CEAS Aeronaut. J.,2017

5. Design and sizing of an aeroelastic composite model for an UCAV configuration with maneuver, gust and landing loads;Bramsiepe,2017

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