Flight Mechanical Challenges of STOL Aircraft Using Active High Lift-Reference-Cited by-同舟云学术

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Flight Mechanical Challenges of STOL Aircraft Using Active High Lift

Published:2019-09 Issue:5 Volume:56 Page:1753-1764
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Diekmann J. H.¹

Affiliation:

1. Institute of Flight Systems, 38108 Braunschweig, Germany

Funder

Deutsches Zentrum für Luft- und Raumfahrt

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference25 articles.

1. NortonB., STOL Progenitors: The Technology Path to a Large STOL Transport and the C-17A, AIAA, Reston, VA, 2002, pp. 22–55.

2. SFB 880: fundamentals of high lift for future commercial aircraft

3. Progress in Efficient Active High-Lift

4. Aircraft and technology for low noise short take-off and landing

5. Flight Dynamics Investigation of an Active High-Lift Aircraft

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1. Unsteady nonlinear lifting line model for active gust load alleviation of airplanes;CEAS Aeronautical Journal;2024-08-05

2. Numerical Study of Flow Control on Simplified High-Lift Configurations;Journal of Applied Fluid Mechanics;2023-04-01

3. Novel Concepts for Active Load Alleviation;AIAA SCITECH 2022 Forum;2022-01-03

4. Understanding the Flight Mechanics of Active High-Lift Aircraft Configurations: Achievements of the CRC 880 Project;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-18

5. Morphing Wing Droop Nose with Large Deformation: Ground Tests and Lessons Learned;Aerospace;2019-10-02

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