Aerodynamic performance assessment of a ducted fan UAV for VTOL applications

S Deng, S Wang, Z Zhang - Aerospace Science and Technology, 2020 - Elsevier
The aerodynamic performance of a recent developed ducted fan Unmanned Aerial Vehicle
(UAV) was experimentally assessed by means of force, pressure and PIV measurements …

Flight dynamics of a morphing aircraft utilizing independent multiple-joint wing sweep

DT Grant, M Abdulrahim, R Lind - International Journal of …, 2010 - journals.sagepub.com
Morphing, which changes the shape and configuration of an aircraft, is being adopted to
expand mission capabilities of aircraft. The introduction of biologically-inspired morphing is …

Time-varying dynamics of a micro air vehicle with variable-sweep morphing

A Chakravarthy, DT Grant, R Lind - Journal of Guidance, Control, and …, 2012 - arc.aiaa.org
MANY studies into morphing aircraft have focused on the steady-state benefits of altering a
configuration for issues such as fuel consumption, range and endurance, cost and logistics …

Design and analysis of biomimetic joints for morphing of micro air vehicles

DT Grant, M Abdulrahim, R Lind - Bioinspiration & biomimetics, 2010 - iopscience.iop.org
Flight capability for micro air vehicles is rapidly maturing throughout the aviation community;
however, mission capability has not yet matured at the same pace. Maintaining trim during a …

An annular wing VTOL UAV: Flight dynamics and control

R Gill, R D'Andrea - Drones, 2020 - mdpi.com
A vertical takeoff and landing, unmanned aerial vehicle is presented that features a
quadrotor design for propulsion and attitude stabilization, and an annular wing that provides …

Analytical Model for Ring-Wing Propulsors at Angle of Attack

MJ Werle - Journal of Aircraft, 2022 - arc.aiaa.org
A simple, accurate, analytical model is developed for predicting the forces and moments on
subsonic ring-wing propulsors (aka fan ducts and shrouded propellers) at angle of attack …

Analytical model for ring-wing propulsor thrust augmentation

MJ Werle - Journal of Aircraft, 2020 - arc.aiaa.org
A simple, accurate, reduced-order model is developed for predicting the maximum available
thrust performance of subsonic ring-wing propulsors varying in shroud airfoil length …

Aerodynamic estimation of annular wings based on leading-edge suction analogy

A Maqsood, TH Go - AIAA journal, 2013 - arc.aiaa.org
ANNULAR wings belong to the class of nonplanar wing configurations and have gained
significant popularity recently [1–5] among the designers of unmanned air vehicles (UAVs) …

Aerodynamic loads and moments on axisymmetric ring-wing ducts

MJ Werle - AIAA Journal, 2014 - arc.aiaa.org
ANALYTICAL methods are discussed and developed for predicting loads and moments on
axisymmetric ducts and ring wings at angles of attack or yaw as depicted in Fig. 1. These are …

Aero-propulsive interaction model for conceptual distributed propulsion aircraft design

M Awad, E Stumpf - Aircraft Engineering and Aerospace Technology, 2022 - emerald.com
Purpose This research aims to present an aero-propulsive interaction model applied to
conceptual aircraft design with distributed electric propulsion (DeP). The developed model …