Effect of Thickness-To-Chord Ratio on Flow Structure of a Low Swept Delta Wing

AIAA Journal- United States

doi 10.2514/1.j057083

Full Text

Abstract

Available in

Date

Authors

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Flow Structure of Critical States for a Rolling Delta Wing

Journal of the Visualization Society of Japan
2002English

Unsteady Flow Structure on Low Aspect Ratio Wings

2011English

Numerical Simulation of Shock-Stall Flutter of a High-Aspect-Ratio Forward-Swept Wing

Transactions of the Japan Society for Aeronautical and Space Sciences
SpacePlanetary ScienceAerospace Engineering
2013English

Unconventional High Aspect Ratio Joined-Wing Aircraft With Aft- And Forward-Swept Wing-Tips

2003English

A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying Wing to Improve Lift Performance

International Journal of Micro Air Vehicles
Aerospace Engineering
2015English

Experimental Control of Swept-Wing Transition Through Base-Flow Modification by Plasma Actuators

Journal of Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2018English

Effect of Aerodynamic Configuration Parameters on Lateral-Directional Stability of Double-Swept Flying Wing Aircraft

Journal of Aerospace Technology and Management
Aerospace Engineering
2019English

Flow Behavior in Side-View Plane of Pitching Delta Wing

EPJ Web of Conferences
AstronomyPhysics
2018English

Flow Structures in End-View Plane of Slender Delta Wing

EPJ Web of Conferences
AstronomyPhysics
2017English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy