Verification of a Flying Wing Handling Qualities Analysis by means of In-Flight Simulation-Reference-Cited by-同舟云学术

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Verification of a Flying Wing Handling Qualities Analysis by means of In-Flight Simulation

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Ehlers Jana¹,Niedermeier Dominik¹,Leissling Dirk¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6540

Reference13 articles.

1. ur Rahman, N. "Propulsion and Flight Controls Integration for the Blended Wing Body Aircraft", Ph.D. Thesis,Department of Aerospace Sciences, Cranfield University, May 2009

2. The longitudinal flying qualities of a blended-wing-body civil transport aircraft

3. Stability and Control Assessment of a Blended-Wing-Body Airliner Configuration

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2. Simulator Assessment of the Lateral-Directional Handling Qualities of the Flying-V;AIAA SCITECH 2023 Forum;2023-01-19

3. In-Flight Simulator VFW 614 ATTAS;In-Flight Simulators and Fly-by-Wire/Light Demonstrators;2017

4. Review of evolving trends in blended wing body aircraft design;Progress in Aerospace Sciences;2016-04

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