Aerodynamic Assessment of a Control Strategy Based on Twist Morphing Wing in a Flying Wing Aircraft-Reference-Cited by-同舟云学术

Aerodynamic Assessment of a Control Strategy Based on Twist Morphing Wing in a Flying Wing Aircraft

Published:2024-01 Issue:1 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Karimi Kelayeh Ruhollah¹,Djavareshkian Mohammad Hasan²^ORCID

Affiliation:

1. Postgraduate Researcher, Dept. of Mechanical and Aerospace Engineering, Faculty of Engineering, Ferdowsi Univ. of Mashhad, Azadi Square, Mashhad 9177948974, Iran.

2. Professor, Dept. of Mechanical and Aerospace Engineering, Faculty of Engineering, Ferdowsi Univ. of Mashhad, Azadi Square, Mashhad 9177948974, Iran (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5073

Reference41 articles.

1. Flight Characteristics of Shaping the Membrane Wing of a Micro Air Vehicle

2. Twist Morphing Using the Variable Cross Section Spar: Feasibility Study

3. Barnard, R. H., and D. R. Philpott. 2010. Aircraft flight: A description of the physical principles of aircraft flight. London: Pearson Education.

4. Flying wing—problems and decisions

5. Effect of sweep angle on the vortical flow over delta wings at an angle of attack of 10;Brett J.;J. Eng. Sci. Technol.,2014

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