Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1980-03-28
1981-09-01
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
042864607
ABSTRACT:
The invention relates to a device which changes the Mach number capability of a wind tunnel without permanently altering the existing nozzle of the tunnel. An insert (14) is removably attached to the wall (17) of the existing nozzle expansion area (22) thereby creating a second minimum section (15) upstream of the model test section (21). The added insert (14) may be removed without complicated and expensive changes to the basic wind tunnel. In the embodiment illustrated in FIG. 2, a removable insert (25) is disposed within wind tunnel nozzle walls (17) with a portion of the flow boundary layer being bled off from the tunnel via passageway (29) and tunnel exit (28) to thereby reduce the extent of separated flow normally occuring upstream of the insert contraction section.
REFERENCES:
patent: 3011341 (1961-12-01), Hill
Manning John R.
Nelson Wallace J.
Osborn Howard J.
The United States of America as represented by the Administrator
Woodiel Donald O.
LandOfFree
Wind tunnel supplementary Mach number minimum section insert does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Wind tunnel supplementary Mach number minimum section insert, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Wind tunnel supplementary Mach number minimum section insert will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1670168