Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests

Journal of Aircraft - United States
doi 10.2514/1.c033909
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Combined Droop Nose and Trailing-Edges Morphing Effects on Airfoils Aerodynamics

SN Applied Sciences
2019English

Static and Fatigue Tests of F-111b Boron Wing Tip

1975English

Conceptual-Level Evaluation of a Variable Stiffness Skin for a Morphing Wing Leading Edge

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Mechanical EngineeringAerospace Engineering
2019English

Development of a Morphing Wingtip Based on Compliant Structures

Journal of Intelligent Material Systems and Structures
Materials ScienceMechanical Engineering
2018English

Experimental Investigation of Wing Tip Vortices in the Near-Field

EPJ Web of Conferences
AstronomyPhysics
2019English

Numerical and Experimental Investigation of the Reduction of Hypersonic Nose Tip Ablation

1998English

Span Morphing Using the GNATSpar Wing

Aerospace Science and Technology
Aerospace Engineering
2016English

Conceptual Design of Deployment Structure of Morphing Nose Cone

Advances in Mechanical Engineering
Mechanical Engineering
2013English

Pressure Deflection Behavior of Candidate Materials for a Morphing Wing

English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy