Services

EXPERIMENTAL

Wind Tunnel Testing
  • Preparation of Test Plans
  • Preparation of Cost Estimates
  • Pre-Test Activities/Meetings
  • Test Justification Presentations
  • Instrumentation Plans and Specifications
  • Instrumentation Staging and Setup
  • On-site Principal Investigator Team
  • Monthly Status/Progress Reporting and Cost Accounting
  • Post-Test Analysis
  • Preparation and Submission of Final Reports
Aircraft Modification/Design
  • Preparation of Conceptual Designs
  • Preparation of Ultimate/Limit Loads for Modification
  • Preparation for and Completion of Ground "Static" tests
  • Conduct of Flight Tests
Flight Testing
  • Preparation of Test Plans
  • Preparation of Ultimate/Limit Loads for Aircraft Modification
  • Preparation of Cost Estimates
  • Instrumentation Plans and Specifications
  • Instrumentation Staging and Setup
  • Airworthy Instrumentation Installation
  • Ground Testing/Pre-Flight Checkouts
  • On-site Principal Investigator Team
  • Flight-Qualified Personnel (FAA Flight Physical, High-Altitude Chamber, etc.)
  • Monthly Status/Progress Reporting and Cost Accounting
  • Post-Test Analysis
  • Preparation and Submission of Final Reports
Wind Tunnel Facilities Used
  • 11-ft. by 11-ft. TWT, NASA-Ames
  • 12-ft. PWT, NASA-Ames
  • 9-ft. by 7-ft. SST, NASA-Ames
  • 48-inch Anechoic Jet Facility, NASA-Langley
  • 16T TWT, AEDC
  • 8-ft. Calspan, Buffalo
  • 6-ft. by 8-ft. Trisonic, North American Aviation, LAX
  • 2-ft. by 2-ft. TWT, Wright Labs, Ohio
Aircraft Used
  • 747-100/200
  • ER-2
  • 747SP
  • U-2
  • KC-135
  • C-141
  • WB-57
  • 767
  • A-3
  • G-IIB
Types of Testing
  • Turbulence in Tunnel Circuits (Flow Quality)
  • Turbulence in Boundary and Shear Layers
  • Shock Wave/Boundary Layer Interactions
  • Boundary Layer Transition
  • Optical Effect of Aerodynamic Flows
  • Lift/Drag Testing
  • Effect of Fairings/Aircraft Modifications
COMPUTATIONAL

Types of Computational Studies
  • Analysis and Design using Full Navier-Stokes Codes (OVERFLOW)
  • Flow Over Fairings/Cavities
  • Supersonic Inlet Analysis/Design (including the Subsonic Diffuser)
  • Hypersonic Inlet Analysis/Design (through the Scramjet)
Computational Facilities Used
  • IBM 7094
  • CRAY
  • BM 360
  • CRAYII
  • CDC 6600
  • CRAY C90/4 (NAS)
  • CDC 7600
  • SGI Workstations
ADMINISTRATIVE
  • Proven Record of Performance
  • DCAA-Consistent Cost Accounting
  • DCAA Audit Survivor (FFP and CPFF)
  • Contract Performance/Schedule/Cost Tracking
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P.O. Box 5146 || Incline Village, NV 89450
Phone: 775.831.5094