Sensitivity Analysis of Counterflow Thrust Vector Control with a Three-Dimensional Rectangular Nozzle-Reference-Cited by-同舟云学术

Sensitivity Analysis of Counterflow Thrust Vector Control with a Three-Dimensional Rectangular Nozzle

Published:2021-01 Issue:1 Volume:34 Page:04020107
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wu Kexin¹,Kim Taeho²,Kim Heuydong³

Affiliation:

1. Researcher, Dept. of Mechanical Engineering, Andong Univ., 1375, Gyeongdong (SongCheon-dong), Andong, Gyeongsangbuk-do 36729, South Korea-100038.

2. Research Professor, Dept. of Mechanical Engineering, Andong Univ., 1375, Gyeongdong (SongCheon-dong), Andong, Gyeongsangbuk-do 36729, South Korea-100038.

3. Full Professor, Dept. of Mechanical Engineering, Andong Univ., 1375, Gyeongdong (SongCheon-dong), Andong, Gyeongsangbuk-do 36729, South Korea-100038 (corresponding author).

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.1943-5525.0001228

Reference42 articles.

1. Vectoring Thrust in Multiaxes Using Confined Shear Layers

2. Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet

3. An investigation of empirical formulation and design optimisation of co-flow fluidic thrust vectoring nozzles

4. THE AEROACOUSTICS AND AERODYNAMICS OF HIGH-SPEED COANDA DEVICES, PART 1: CONVENTIONAL ARRANGEMENT OF EXIT NOZZLE AND SURFACE

5. Computational Fluid Dynamic Study on a Novel Propulsive System: ACHEON and Its Integration with an Unmanned Aerial Vehicle (UAV)

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