Mr. Weidong Yang Profile

Weidong Yang

SPIE Involvement:

Author

Publications (1)

This will count as one of your downloads.

You will have access to both the presentation and article (if available).

DOWNLOAD NOW

This content is available for download via your institution's subscription. To access this item, please sign in to your personal account.

Email or Username Forgot your username?

Password Forgot your password?

Show

Keep me signed in

No SPIE account? Create an account

Proceedings Article | 11 October 2023 Paper

Numerical simulation study on wall interference of multi-size wind tunnel

Na Gao, Weidong Yang, Honglei Ma

Proceedings Volume 12800, 128000B (2023) https://doi.org/10.1117/12.3003962

KEYWORDS: Numerical simulations, Wind measurement, Computer simulations, Aerodynamics, Data modeling, Resistance, Instrument modeling, 3D modeling, Sodium, Quality testing methods

Read Abstract +

Wind tunnel experiment plays a very important role in the development of aircraft, but the existence of wind tunnel wall has a significant interference effect on the aerodynamic characteristics of aircraft, so it is necessary to do relevant research on the interference of tunnel wall. According to the characteristics of wind tunnel experiment, the flow field of a standard model in unsupported state in medium-sized wind tunnel open test section, medium-sized wind tunnel closed test section, large-sized wind tunnel closed test section and free flow field is numerically simulated By analyzing the variation of lift coefficient interference and drag coefficient interference with angle of attack, the following conclusions are obtained: the lift interference laws of the two sizes of closed wind tunnels are similar, and the interference increases with the increase of angle of attack, reaching the maximum when the angle of attack is 60 degrees, and then decreasing after the angle of attack is 60 degrees, and the lift interference of the open wind tunnel is the smallest, and the maximum appears at the angle of attack of 80 degrees. The law of resistance interference in closed wind tunnels with two sizes is similar, and the interference amount increases with the increase of angle of attack, while the resistance interference amount in open wind tunnels is the smallest. The outer boundary of the main flow area in the upstream of the aircraft is basically the same at different angles of attack, and in the downstream of the aircraft, the outer boundary of the main flow area gradually increases with the increase of angle of attack.

My Library

You currently do not have any folders to save your paper to! Create a new folder below.

Folder Name

Folder Description

View contact details

UPDATE YOUR PROFILE

Is this your profile? Update it now.

Sign into your SPIE.org account

Don’t have a profile and want one?

Create an account on SPIE.org

Access to the requested content is limited to institutions that have purchased or subscribe to SPIE eBooks. You are receiving this notice because your organization may not have SPIE eBooks access.*

*Shibboleth/Open Athens users─please sign in to access your institution's subscriptions.

To obtain this item, you may purchase the complete book in print or electronic format on SPIE.org.

ORGANIZATIONAL
Sign in with credentials provided by your organization.

Organizational Username

Organizational Password

Show/Hide Password

INSTITUTIONAL
Select your institution to access the SPIE Digital Library.

SELECT YOUR INSTITUTION

PERSONAL
Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.

PERSONAL SIGN IN

No SPIE Account? Create one

PURCHASE THIS CONTENT

SUBSCRIBE TO DIGITAL LIBRARY

50 downloads per 1-year subscription

Members: $195

Non-members: $335 ADD TO CART

25 downloads per 1 - year subscription

Members: $145

Non-members: $250 ADD TO CART

PURCHASE SINGLE ARTICLE

Includes PDF, HTML & Video, when available

Members:

Non-members: ADD TO CART

Keywords/Phrases

Search In:

Publication Years