My WebLink
|
Help
|
About
|
Sign Out
Home
Browse
Search
WMOD00284
CWCB
>
Weather Modification
>
DayForward
>
WMOD00284
Metadata
Thumbnails
Annotations
Entry Properties
Last modified
7/28/2009 2:32:39 PM
Creation date
1/8/2008 12:16:50 PM
Metadata
Fields
Template:
Weather Modification
Applicant
Thompson, J.R., G.W. Wilderson, and D.A. Griffith, North American Weather Consultants
Sponsor Name
USBR
Title
Cloud Seeding Data Collection, and Analysis Assoc. with the Colo River Augmentation Demonstration Program
Prepared For
USBR, Divison of Atmospheric Research
Prepared By
Thompson, Wilderson, Griffith
Date
12/1/1987
State
AZ
Weather Modification - Doc Type
Scientific Study
Jump to thumbnail
< previous set
next set >
There are no annotations on this page.
Document management portal powered by Laserfiche WebLink 9 © 1998-2015
Laserfiche.
All rights reserved.
/
251
PDF
Print
Pages to print
Enter page numbers and/or page ranges separated by commas. For example, 1,3,5-12.
After downloading, print the document using a PDF reader (e.g. Adobe Reader).
Show annotations
View images
View plain text
<br />I <br />I <br />I <br />I <br />I <br />, <br />I <br />I <br /> <br />The prlmary purpose of the SF6 measurements was to simulate <br />the transport and diffusion of seeding materials from either <br />a ground based, or airborne source. During the 1987 field <br />season all releases did occur from ground level. Once a plume <br />was intersected then the objective was to obtain data on the <br />conditions of the parcel of air in which it resided. In partic- <br />ular, the frequency of occurrence, amount, -and spatial distribu- <br />tions of supercooled liquid water, the ambient alr temperature, <br />stability, and other meteorological conditions which affect <br />the production and/or depletion of supercooled liquid water <br />were examined, The assessment of various cloud seeding techniques <br />over and around orographic barriers was also examined by observing <br />the transport and dispersion patterns of the SF6 gas. <br /> <br />I <br />1 <br />I <br />t <br />l <br /> <br />4.2 Description of Equipment <br /> <br />l <br /> <br />The continuous SF6' analyzer designed by Washington state <br />University (Benner, and Lamb, 1985) and manufactured by Scientech, <br />pullman, Washington was utilized on board the University of <br />wyoming's high performance King Air aircraft. The analyzer <br />was mounted in a rack along with one cylinder of ultra-pure <br />nitrogen and one cylinder of hydrogen, both necessary to operate <br />the analyzer. In addition, an external pump was used to draw <br />ln ambient air through a port located in the top right section <br />of the fuselage, through approximately ten feet of 1/8 inch <br />teflon tubing, and then injected into the inlet port of the <br />analyzer. The lag time through this ten foot section of tubing <br />was measured on the ground by releasing an excess flow of <br />95 ppt calibration gas into the port on the outside of the <br />plane, and then measuring the lag time between injection and <br />response. This lag time was found to be approximately three <br />seconds. <br /> <br />t <br />i <br /> <br />1 <br /> <br />4-5 <br /> <br />j <br /> <br />1_ <br />
The URL can be used to link to this page
Your browser does not support the video tag.