Wing-Body and Vertical Tail Interference Effects on Downwash Rate of the Horizontal Tail in Subsonic Flow-Reference-Cited by-同舟云学术

Wing-Body and Vertical Tail Interference Effects on Downwash Rate of the Horizontal Tail in Subsonic Flow

Published:2017-07 Issue:4 Volume:30 Page:04017001
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Paziresh Ali¹,Nikseresht Amir Hossein²,Moradi Hashem³

Affiliation:

1. Graduate Student, Dept. of Mechanical and Aerospace Engineering, Shiraz Univ. of Technology, Modaress Blvd., 7155713876 Shiraz, Iran.

2. Associate Professor, Dept. of Mechanical and Aerospace Engineering, Shiraz Univ. of Technology, Modaress Blvd., 7155713876 Shiraz, Iran (corresponding author).

3. Graduate Student, Dept. of Ocean Engineering, Amirkabir Univ. of Technology, Hafez St., 158754413 Tehran, Iran.

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.1943-5525.0000704

Reference23 articles.

1. Boschetti P. J. Cardenas E. M. and Amerio A. (2012). “Induced drag reduction of an airplane using local twist panel method verification.” 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition AIAA Nashville TN.

2. Introduction to Aeronautics

3. Effects of wing geometry on wing-body-tail interference in subsonic flow

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