Tip Clearance Investigation of a Ducted Fan Used in VTOL UAVS: Part 1—Baseline Experiments and Computational Validation

doi 10.1115/gt2011-46356
Full Text
Abstract

Available in full text

Date
Authors
Publisher

ASMEDC

Related search

Tip Clearance Investigation of a Ducted Fan Used in VTOL UAVS: Part 2—Novel Treatments via Computational Design and Their Experimental Verification

2011English

Lip Separation and Inlet Flow Distortion Control in Ducted Fans Used in VTOL Systems

2014English

Modelling, Attitude Controller Design and Flight Experiments of a Novel Micro-Ducted-Fan Aircraft

Advances in Mechanical Engineering
Mechanical Engineering
2018English

Design and Construction of a Small Ducted Fan Engine for Nonlinear Control Experiments

English

Tip Leakage Flow and Heat Transfer on Turbine Blade Tip and Casing, Part 1: Effect of Tip Clearance Height and Rotation Speed

International Journal of Computational Methods in Engineering Science and Mechanics
Computational MechanicsComputational Mathematics
2013English

Computational Investigation of Aerodynamic Characteristics for Elliptic UAVs’ Wing

Asian Journal of Engineering and Technology
2018English

Noise Source Identification for Ducted Fan Systems

2007English

Numerical Investigation of Acoustics Performance of Low- Pressure Ducted Axial Fan by Using Different Turbulence Models

ITM Web of Conferences
2018English

Experimental Investigation of a Low Hub-To-Tip Ratio Single Stage Transonic Fan

1981English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy