Optimization and Analysis of a Blown Flap Based on a Multielement Airfoil-Reference-Cited by-同舟云学术

Optimization and Analysis of a Blown Flap Based on a Multielement Airfoil

Published:2020-01 Issue:1 Volume:57 Page:62-75
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Yuhui Yin¹,Yufei Zhang¹

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

Funder

Key Laboratory of Aerodynamic Noise Control

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference36 articles.

1. JohnsonG. “Some Recent Aerodynamic Advances in STOL Aircraft,” AIAA Paper 1964-0183, 1964. doi:10.2514/6.1964-183

2. Hydrodynamic characteristics of seaplanes as affected by hull shape parameters

3. Aerodynamic Installation Effects of an Over-the-Wing Propeller on a High-Lift Configuration

4. CampbellJ. P.JohnsonJ. L. Jr, “Wind-Tunnel Investigation of an External Flow Jet-Augmented Slotted Flap Suitable for Application to Airplanes with Pod-Mounted Engines,” NASA TN-3898, 1956.

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