Wind tunnel and collector configuration therefor

Details Wind tunnel and collector configuration therefor Wind tunnel and collector configuration therefor

2006-02-14

2006-02-14

Lefkowitz, Edward (Department: 2855)

Measuring and testing

Wind tunnel: aerodynamic wing and propeller study

Reexamination Certificate

active

06997049

ABSTRACT:
An open jet wind tunnel having a test section, a nozzle exit and a collector in which the leading edge of the collector is configured with at least a portion being non-uniformly spaced from the nozzle exit.

REFERENCES:
patent: 5025659 (1991-06-01), Starr, Jr. et al.
patent: 5341676 (1994-08-01), Gouterman et al.
patent: 5405106 (1995-04-01), Chintamani et al.
patent: 5435175 (1995-07-01), Kramer et al.
patent: 6725912 (2004-04-01), Moll et al.
patent: 2003/0070479 (2003-04-01), Lacey, Jr.
patent: 05026762 (1993-02-01), None
patent: 06201512 (1994-07-01), None
patent: WO 89/03977 (1989-05-01), None
K.K. Ahuja, “Aeroacoustic Performance of Open-Jet Wind Tunnels with Particular Reference to Jet/Collector Interactions”, GTRI Project A-9730, May 1994-Oct. 1994, 25pgs.
Rennie, Mark, “Effect of Jet Length on Pressure Fluctuations in ¾ Open-Jet Wind Tunnels”, Internet Article, www.aiolos.com
ews/paperspublished.asp, Nov. 5, 2002 (8pgs).

Affiliated with

Also associated with

Rating

Wind tunnel and collector configuration therefor 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 and collector configuration therefor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Wind tunnel and collector configuration therefor will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3645615