AIAA GTTC HANDBOOK
SECTION VII – WORKING GROUPS (This page is under construction)
Working Group
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Working
Group Summary Presentations from the Portland, OR - GT Conference 2004 :
Click Here (2.4MB Zip file, MS Powerpoint
2002 Format)
Working Groups were developed
under the GTTC in order to address specific technical issues of interest to the
ground testing community. The idea
for a specific Working Group comes from either inside the GTTC or from
recommendations outside the GTTC.
For any Working Group to be formed, a GTTC member must become its
champion and chair. The Working
Group must develop a charter (similar to a Task Subcommittee Charter) that
details its operation and objectives. A Working Group differs from a Task Subcommittee in that:
Timeline for GTTC Working Group
Operation: As mentioned above, a
GTTC Working Group is chaired and championed by a GTTC member (although
non-GTTC members can be involved in championing a new Working Group, as
well). The process and approximate
timeline for establishing and operating a Working Group is described below:
·
As noted, the Working Group Chair must be a GTTC
member. Other Working Group
officers (vice-chair, secretary) are not required to be GTTC members.
·
If, following the organization and setup of a proposed
Working Group, the GTTC membership feels that a proposed Working Group has merit,
but has not provided an adequate charter or plan, the GTTC can reject the
proposed Working Group or allow the proposed Working Group one additional
planning meeting to revise the charter and plan.
·
The active period for a Working Group may last 5 years
or longer, depending on the scope of the Working Group objectives.
·
If the primary goal of the Working Group is the
development of an AIAA Standards document, then some coordination/communication
with the GTTC Standards Subcommittee is warranted to insure that proper document review and approval
procedures are followed.
·
If a Working Group is developing an AIAA standards
document, the Working Group will usually switch to inactive status after the
draft standards document has been reviewed by a peer review team, the comments
of that review have been incorporated back into the draft document, and the
document has been approved by the GTTC membership.
·
During the inactive phase, the Working Group chair (or
designee) will act as the point-of-contact with AIAA while AIAA reviews and
publishes the document.
·
A Working Group will remain on inactive status until
the final document is published by AIAA.
·
If necessary, the Working Group can hold occasional
meetings while on inactive status.
·
The Working Group chair, though now not a GTTC member,
will be the point-of-contact with the GTTC.
·
A Working Group will remain on casual status as long as
any standard document produced by that Working Group is being maintained by the
AIAA.
The GTTC has had great success
through its Working Groups, and for the benefit of future Working Groups, the
GTTC has developed a list of lessons learned in
the formation and operation of Working Groups:
The following is a summary of the
GTTC Working Groups:
·
Current Working Groups:
§
Chair: Frank Steinle (Sverdrup Technology/AEDC)
o
Thrust Stands
§
Chair: Ray Castner (NASA Glenn)
·
Working Groups under construction:
o
Test Nomenclature
§
Champion:
Jerry Kegelman (NASA Langley)
o
Dynamic Testing
§
Champion:
Greg Addingtion (AFRL)
·
Working Groups that have completed their assigned
tasks:
o
Internal
Balances Technology
§
Chair:
David Cahill (Sverdrup Technology / AEDC)
§
Final Product:
AIAA Recommended Practice document AIAA R-091-2003
Calibration and
Use of Internal Strain-Gage Balances
AIAA R-091-2002, 6x96 Matrix Computation
Example
§
Chair:
Mark Melanson (Lockheed Martin)
§
Final Product:
Two-Volume AIAA Recommended Practice document AIAA R-092-2003
Recommended
Practice for Successful Wind Tunnel Testing
Vol. I. Management Guide
Vol. II.
Practitioners Volume
o
Wind Tunnel Calibration Methodology
§
Chair:
Allen Arrington (QSS Group, Inc. / NASA Glenn)
§
Final Product:
AIAA Recommended Practice document AIAA R-093-2003
Calibration of
Subsonic and Transonic Wind Tunnels
AEROSPACE TEST PROCESSES
WORKING GROUP
SCOPE
The Aerospace Test Processes Working Group is assembled to document best
practices associated with wind tunnel testing as a way to recommend improvements
in wind tunnel test efficiency, costs, and cycle time. It is the resolve of the
Test Processes membership to discuss and document, in published form, proven
practices/lessons learned that has contributed to the success of the collective
memberships organizations.
STRUCTURE
Members of the GTTC staff the Aerospace Test Processes Working Group as well
as representatives from wind tunnel model suppliers, users, and test facilities
personnel.
OBJECTIVES
OPERATION
INTERNAL BALANCE AND CALIBRATION TECHNOLOGY
WORKING GROUP
SCOPE
Internal strain-gage balances are used extensively to measure the aerodynamic
loads on a test article during a wind tunnel test. There has been little collaboration
among the users of internal balances and, as a result, several types of
balances, calibration methods, calibration matrices, tare adjustment, and
uncertainty evaluations have evolved. The time has arrived where a
collaborative effort is needed to advance the state-of-the-art for internal
strain-gage balances and calibration technology. Individuals from wind tunnel
facilities will pool their information and experiences to enhance each others
capabilities and to develop standards for their use, calibration, tare
adjustment, and uncertainty evaluation. The working group is not an opportunity
for an organization to promote their particular balance design, fabrication,
and/or calibration services.
STRUCTURE
The Internal Balance and Calibration Technology Working Group was formed under
the auspices of the AIAA Ground Testing Technical Committee (GTTC). The working
group is staffed by selected volunteers from various wind tunnel facilities and
is not limited to members of the GTTC or AIAA. The Chairperson for the working
group shall be a member of the GTTC and will be appointed by the GTTC
Chairperson. An individual's service on the working group will continue until
the objectives for which they were selected have been completed. Currently,
membership on the working group is limited to individuals from facilities
operated by government or commercial enterprises in the US and Canada.
OBJECTIVES
OPERATION
WIND TUNNEL CALIBRATION WORKING GROUP
SCOPE
Wind tunnels provide a primary source of test data
for basic aerodynamic research and for the design and development of aircraft,
aircraft components and propulsion systems. Due to advances in instrumentation
and data systems that allow for more accurate measurement of the flow
parameters and the increased sensitivity of aerodynamic and propulsion system
performance with wind tunnel flow quality, the accurate calibration of wind
tunnels has become very important. In the past, there have been workshops and
general meetings to discuss issues pertaining to wind tunnel calibration, but
in general, there was no closure or final recommendations produced from these
exercises. The members of the working group will pool their information and
experiences to enhance each others capability in wind tunnel calibration and to
develop standards for tunnel calibration, documentation and presentation of
calibration results and uncertainty analysis.
Due to the large number of variables involved in
wind tunnel testing (Mach number range, size/type of facility, types of
testing, model blockage effects, etc.) it would not be possible to address all
pertinent issues at one time, so the scope of the working group will be focused
on a subset of wind tunnels and test ranges. From discussions with wind tunnel
users/operators from within the GTTC, it was suggested to limit the initial
scope of the working group to subsonic and transonic wind tunnel facilities and
to look only at the aerodynamic calibration of the empty test section of these
types of facilities. The scope of the working group would be changed to cover
other calibration issues (supersonic tunnels, model effects, etc.) as the
initial topics were completed.
STRUCTURE
The Wind Tunnel Calibration Methodology Working
Group was formed under the operating structure of the AIAA Ground testing
Technical Committee (GTTC). The working group will be staffed by
representatives from several wind tunnel facilities and is not limited to
members of the AIAA or GTTC. The Chairperson of the working group shall be a
member of the GTTC and will be appointed by the GTTC Chairperson.
OBJECTIVES
OPERATION
WIND
TUNNEL FLOW QUALITY WORKING GROUP
SCOPE
Thrust
stands are used extensively to measure the propulsive forces generated by a
test article. For a variety of
reasons, several types of thrust stands, calibration methods, tare measurements
and uncertainty evaluations have evolved throughout industry, government and
academia. This group recognizes
the benefits of identifying standards and acceptable practices. It is the intent of the individuals of
this working group to pool their information and experiences to develop a
single source describing the major issues associated with thrust stand design
and operation. The source will
also provide a list of reference material to substantiate and enhance the
group's work. It is hoped that the
scope of the working group will become more focused on these major issues after
the initial overview topic is completed.
STRUCTURE
The
Thrust Stand Working Group was formed under the auspices of the AIAA Ground
Testing Technical Committee (GTTC).
The working group is staffed by selected volunteers from academia,
industry and government and is not limited to members of the GTTC or AIAA. The Chairperson for the working group
shall be a member of the GTTC and will be appointed by the GTTC
Chairperson. An individual's
service on the working group will continue until the objectives for which they
were selected have been completed.
OBJECTIVES
OPERATION
WORKING GROUP DOCUMENTS
Thrust Stand Guide – e-mail Mark.Cross@arnold.af.mil or Raymond.S.Castner@nasa.gov if you
are on the committee and would like access to this document.
E-mail submissions to
Mark.Cross@arnold.af.mil
or Raymond.S.Castner@nasa.gov
This
page was last updated 2/6/2008. Contact Julien Weiss with any
changes.