Combat aircraft agility metrics-a review

AA Paranjape, N Ananthkrishnan - Journal of Aerospace Sciences and …, 2006 - joast.org
With changing combat environments, traditional measures of merit for fighter aircraft
performance have largely proved insufficient to analyze combat capability. Combat …

[HTML][HTML] Maneuver control at high angle of attack based on real-time optimization of integrated aero-propulsion

F Juan, Q Zheng, CAI Changpeng, H Zhang - Chinese Journal of …, 2022 - Elsevier
To reduce the propulsion system installation thrust loss under high angle of attack
maneuvering, a control method based on real-time optimization of the integrated aero …

Steady and unsteady maneuvering forces and moments on slender bodies

KO Granlund - 2009 - vtechworks.lib.vt.edu
Steady and Unsteady Maneuvering Forces and Moments on Slender Bodies Page 1 Steady
and Unsteady Maneuvering Forces and Moments on Slender Bodies Kenneth Granlund …

Im**ement of a von kàrmàn vortex street on a delta wing

I Heron, RY Myose - Journal of aircraft, 2005 - arc.aiaa.org
HIGH-PERFORMANCE military aircraft oftentimes employ delta-shaped wings. It is well
documented that delta wings at a fixed angle of attack generate lift by separating a shear …

Chaotic analysis and control of longitudinal flight dynamics

L Su, H Yao, J Du - Asian Journal of Control, 2015 - Wiley Online Library
Aircraft are considered to be sub‐stable within the flight envelope. This paper presents a
chaotic analysis and two kinds of corresponding control methods of aircraft longitudinal flight …

Delta wing vortex-burst behavior under a dynamic freestream

I Heron, RY Myose - Journal of aircraft, 2009 - arc.aiaa.org
DELTA wings have evolved over the years and are now used primarily in the form of leading-
edge extensions on many fighter aircraft. As these aircraft become more and more …

Vortex Burst Behavior Under Dynamic Freestream

I Heron, R Myose - 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005 - arc.aiaa.org
A series of experiments on a 70-degree delta wing was conducted at Wichita State
University to study the effect on the vortex burst position when simultaneous dynamic pitch …

Im**ement of a von Kà rmà n Vortex Street on a Dynamically Pitching Delta Wing

I Heron, R Myose - 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006 - arc.aiaa.org
A series of experiments on a 70-degree delta wing was conducted at Wichita State
University to study the effect on the vortex burst position of the leading-edge vortices when …

Flying Wing UAV's Maneuver Flight Control Based on Coupling Dynamics Mechanism Analyses

N Zhang, R Ma - Advances in Guidance, Navigation and Control …, 2021 - Springer
Based on mechanism research of dynamic coupling and inertial coupling of flying wing UAV
at high attack angle or stall maneuver flight, a decoupling compensator is designed to …

Im**ement of a von Kà rmà n Vortex Street on a Dynamically Pitching Delta Wing Part 2: Small Cylinder Results

R Myose, I Heron - 47th AIAA Aerospace Sciences Meeting including …, 2009 - arc.aiaa.org
Recent interest in highly maneuverable military aircraft, capable of operating over a large
range of angles of attack, has refocused attention on delta-shaped wings. One of the …