Andere Kunden interessierten sich auch für
![Small Internal Combustion Engine Testing for a Hybrid-Electric Remotely-Piloted Aircraft]( "Small Internal Combustion Engine Testing for a Hybrid-Electric Remotely-Piloted Aircraft")
Small Internal Combustion Engine Testing for a Hybrid-Electric Remotely-Piloted Aircraft54,99 €![Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis]( "Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis")
Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis54,99 €![Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design]( "Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design")
Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design54,99 €![Understanding Schedule Forecasting Shortfalls in Federal Design-Build Facility Procurement]( "Understanding Schedule Forecasting Shortfalls in Federal Design-Build Facility Procurement")
Understanding Schedule Forecasting Shortfalls in Federal Design-Build Facility Procurement58,99 €![A Verification and Validation Assessment of Rapid Availability Prototyping for Testing Operational Readiness]( "A Verification and Validation Assessment of Rapid Availability Prototyping for Testing Operational Readiness")
A Verification and Validation Assessment of Rapid Availability Prototyping for Testing Operational Readiness54,99 €![Analysis of the Application of a Triggered Isomer Heat Exchanger as a Replacement for the Combustion Chamber in an Off-the-Shelf Turbojet]( "Analysis of the Application of a Triggered Isomer Heat Exchanger as a Replacement for the Combustion Chamber in an Off-the-Shelf Turbojet")
Analysis of the Application of a Triggered Isomer Heat Exchanger as a Replacement for the Combustion Chamber in an Off-the-Shelf Turbojet54,99 €![Role of Relatively Small-Scale Force Contributions in Multinational Operations]( "Role of Relatively Small-Scale Force Contributions in Multinational Operations")
Role of Relatively Small-Scale Force Contributions in Multinational Operations59,99 €
This study investigated the design parameters necessary for the construction and use of a testing facility built to evaluate advanced combustor designs for future gas turbine engines. User inputs were acquired by interview and by evaluating facilities at other organizations and used in the decisions made in the accuracy, capability, safety and flexibility of pieces of machinery and how different systems were to interact. All systems and measurements are designed to be compliant with the guidance set forth in SAE ARP 1256. Safeguard systems were also designed into the facility to maintain a safe work environment for the user. These safeguards include automatic fuel shut-offs, heater shut-offs, and general system power downs. While the system is designed to evaluate the testing of a planar 2-D section of the UCC, the labs now have the capability to analyze many systems. The facility, now built, has the ability to supply up to 260 SCFM of air in two legs with 200 SCFM and 60 SCFM splits. These air lines can be independently heated up to 500 -F. The testing area can flow both liquid and gaseous fuels, with a maximum flow rate of 340 mL/min for liquid fuels and 200 SLPM for gaseous fuels. The air flow and fuel flows combine to allow equivalence ratios up to 4 for JP-8 fuels. The facility is also capable of testing systems requiring combustion analysis following SAE ARP 1256 for testing of emissions, a system that requires heated air or fuel, a system that requires an exhaust system to pull gasses out of the testing area, or a system that needs open flame. These additional capabilities allow further research to be conducted on site with an ability to report standardized results.