Effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing-Reference-Cited by-同舟云学术

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Effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing

Published:2022-11 Issue: Volume:130 Page:107929
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Koçak Göktuğ^ORCID,Yavuz Mehmet Metin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Recent developments in delta wing aerodynamics;Gursul;Aeronaut. J.,2004

2. Unsteady aerodynamics of nonslender delta wings;Gursul;Prog. Aerosp. Sci.,2005

3. Passive flow control over flexible non-slender delta wings;Taylor,2005

4. The discrete vortices from a delta wing;Gad-El-Hak;AIAA J.,1985

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Control of Flow Structures on Nonslender Delta Wing Utilizing Nozzle-Type Bleeding Slots;AIAA Journal;2024-09-02

2. Method development for estimation of bleed momentum coefficient using surface pressure measurements and in situ hot wire calibration;Flow Measurement and Instrumentation;2024-07

3. Experimental investigation of dynamic ground boundary condition for a non-slender delta wing;CEAS Aeronautical Journal;2024-05-30

4. An adaptive law based online system identification of cropped delta unmanned aerial vehicles from flight tests;Aerospace Science and Technology;2023-10

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