PROBLEM OF INTERFERENCE OF AN OGIVAL BODY OF REVOLUTION WITH THE WIND-TUNNEL STING AND SPECIFIC FEATURES OF COMPUTING THIS PROBLEM

2011 ◽  
Vol 42 (3) ◽  
pp. 321-344 ◽  
Author(s):  
Sergey Mikhailovich Bosnyakov ◽  
Vladimir Viktorovich Vlasenko ◽  
Innokentii Aleksandrovich Kursakov ◽  
Sergey Vladimirovich Mikhaylov ◽  
Jurgen Quest
Keyword(s):  
Wind Tunnel ◽  
Body Of Revolution ◽  
Ogival Body

Note on the velocity and temperature distributions behind a heated body of revolution

1938 ◽  
Vol 34 (3) ◽  
pp. 351-353 ◽  
Author(s):  
S. Goldstein
Keyword(s):  
Wind Tunnel ◽  
Preceding Paper ◽  
Body Of Revolution ◽  
Temperature Distributions ◽  
Heated Body ◽  
Made In

The measurements of Hall and Hislop (see the preceding paper) were made in a wind tunnel considerably less turbulent than has usually been used in such measurements.

Velocity and temperature distributions in the turbulent wake behind a heated body of revolution

1938 ◽  
Vol 34 (3) ◽  
pp. 345-350 ◽  
Author(s):  
A. A. Hall ◽  
G. S. Hislop
Keyword(s):  
Wind Tunnel ◽  
Turbulent Wake ◽  
Body Of Revolution ◽  
Mean Values ◽  
Temperature Distributions ◽  
Heated Body

The distributions of velocity and temperature in the wake behind a heated body of revolution have been determined in a low-turbulence wind tunnel. Difficulty was experienced in obtaining a truly symmetrical wake, and observations have been reduced to mean values, curves of which are given.

Rotary Stability Derivatives from Distorted Models

1956 ◽  
Vol 60 (549) ◽  
pp. 623-624
Author(s):  
D. J. Foster ◽  
G. W. Haynes
Keyword(s):  
Boundary Layer ◽  
Wind Tunnel ◽  
Experimental Technique ◽  
Practical Significance ◽  
Body Of Revolution ◽  
Aerodynamic Forces ◽  
Stability Derivatives ◽  
Aerodynamic Derivatives ◽  
Constant Direction ◽  
Model Aircraft

This note is presented as an idea to be criticised rather than as a description of a fully developed experimental technique. There are weaknesses in the method which will prevent it from giving absolutely correct answers, for example, the twist imparted to the boundary layer when a body of revolution is rolled cannot be represented. But some of the major effects can be represented, and the idea may possibly be developed to be of practical significance.It is standard wind tunnel practice to measure the aerodynamic derivatives CYβ, C1β, Cnβ, CMβ, CLβ and CDβ by having a wind stream of constant direction, and measuring aerodynamic forces and moments on a model aircraft placed at angles of yaw and pitch to the stream.

Automated Fiber Placement of Composite Wind Tunnel Blades: Process Planning and Manufacturing

2019 ◽  
Author(s):  
Ramy Harik ◽  
Joshua Halbritter ◽  
Dawn Jegley ◽  
Ray Grenoble ◽  
Brian Mason
Keyword(s):  
Wind Tunnel ◽  
Process Planning ◽  
Fiber Placement ◽  
Automated Fiber Placement
Sign in / Sign up

Export Citation Format

Share Document