Numerical Investigations for Passive and Active Flow Control on Tiltrotor–Wing Aerodynamic Interactions-Reference-Cited by-同舟云学术

Numerical Investigations for Passive and Active Flow Control on Tiltrotor–Wing Aerodynamic Interactions

Published:2021-11 Issue:6 Volume:34 Page:04021094
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhao Guoqing¹,Zhao Qijun²,Li Peng³,Wang Bo¹

Affiliation:

1. Lecturer, National Key Laboratory of Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

2. Professor, National Key Laboratory of Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author).

3. Engineer, National Key Laboratory of Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001288

Reference21 articles.

1. Beck S. 2013. “Full-scale tilt rotor download reduction.” M.S. thesis Dept. of Aerospace and Mechanical Engineering Univ. of Arizona.

2. Compressible Dynamic Stall Control Using a Variable Droop Leading Edge Airfoil

3. Wing Download Results from a Test of a 0.658-Scale V-22 Rotor and Wing

4. Aerodynamic Interactions Between a Rotor and Wing in Hover

5. Grife R. A. Darabai and I. Wygnanski. 2002. “Download reduction on a three-dimensional V-22 model using active flow control.” In Proc. 1st Flow Control Conf. Reston VA: American Institute of Aeronautics and Astronautics.

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