0410-05 -SOW_rev 1.docx
DOCX document 31 KB Posted
- Attached to
- Wind Tunnel Testing Federal contract opportunity
- Solicitation number
- N0017823Q6803
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| 23Q6803_Released.pdf |
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
EXPERIMENTAL GAP-CAVITY SUPPORT BOEING/AFOSR MACH-6 QUIET TUNNEL TESTING STATEMENT OF WORK (SOW)
1.0 BACKGROUND
Research is needed to characterize the response and flow dynamics around a body where a structural failure has occurred. This work expands upon previous test plan developed. The research envisioned here characterizes the failure as a geometrical feature that is simple to describe as an opening in the flow surface. This opening can be idealized as a round hole or an azimuthal slot that leads to a cavity inside the body.
| 2.0 | APPLICABLE DOCUMENTS |
| 2.1 | Test Geometry Configuration Document (attached); and |
| 2.2 | Test Plan (attached). |
| 3.0 | SCOPE OF WORK |
| 3.1 | The Contractor shall collaborate with NSWCDD to prepare for gap-cavity testing at the Tri-Sonic Wind Tunnel at the University of Mississippi. |
| 3.2 | The Contractor shall coordinate with NSWCDD TPOCs for pre-test planning and to establish instrumentation, measurement criteria, define performance metrics, and test plan set up. |
| 3.3 | The Contractor shall test seven (7) geometry configurations with one (1) to three (3) experimental runs per geometry. |
| 3.3.1 | The Contractor shall ensure that the Test geometry configurations is in accordance with the test geometry configuration document. |
| 3.4 | The Contractor shall provide instrumentation necessary to observe phenomena as follows: |
| 3.4.1 | The experimental research is targeted toward four objectives, listed in descending order of importance: 1. Observe local thermal and structural affects around and in a cavity during hypersonic wind tunnel testing; 2. Observe surface heat flux in the mid section around the gap/cavity feature; 3. Observe changes in fluid-structure interaction; and 4. Observe global changes in aerodynamic forces. |
| 3.5 | The Contractor shall support up to ten (10) days of testing for up to four (4) different test geometries. |
| 3.6 | The Contractor shall coordinate with the technical points of contact identified below to accomplish this work. |
| 4.0 | DATA DELIVERABLES |
| 4.1 | The Contractor shall provide data IAW CDRL A001. |
| 5.0 | PERIOD OF PERFORMANCE |
The period of performance is a nine (9) months after receipt of the order.
6.0 TRAVEL REQUIREMENTS
No travel is required.
7.0 SECURITY
All work to be performed under this SOW is unclassified.
8.0 TECHNICAL POINTS OF CONTACT (TPOC)
File details come from the government source that posted it. Updated .