Add to ORKGThe cold gas Subscale Test Facility (SSTF) P6.2, located at the German Aerospace Center DLR in Lampoldshausen is used to test nozzles, diffusers and ejectors in an easy, quick, reliable and effective way with gaseous nitrogen. Some experimental set-ups with nozzles, diffusers and ejectors will be shown. Additional, visualisation technique with an infrared camera and colour Schlieren of the SSTF will be illustrated. Comparison to CFD programs and mathematical models are indicated
The DLR Bremen with the Kryo Lab as testing facility provides the service of both static and dynamic...
DLR arc heated facility LBK with the two test legs L2K (1 MW) and L3K (6 MW) has been improved and m...
The M3 test field at DLR Lampoldshausen has been in service for research and technology development ...
This handbook sets forth criteria for the design, analysis, quality assurance, and documentation of ...
In combination with flight testing and computational fluid dynamics (CFD) schemes, ground based test...
Results of an ongoing collaboration between the engine manufacturer MTU and the German aerospace res...
Results of an ongoing collaboration between the engine manu-facturer MTU and the German aerospace re...
The Institute of Space Propulsion of the German Aerospace Center (DLR) has developed and set up a re...
The High Vacuum Test Facility STG enables an experimental investigation of thruster plumes to determ...
The paper reports the current status of a DLR Lampoldshausen project towards the design, erection, a...
The increasing interest in hypersonic transportation for both civil and military use results in an i...
New Siemens burner concepts thought to produce a more homogeneous air/fuel mix-ture and a better dis...
Within a joint research effort of Astrium and DLR, cold-gas test campaigns with subscale nozzles wer...
The objectives of this research were to build a facility that could simulate the expected fluid flow...
As part of FLPP3 tests about the stratification with liquids in very low temperature regions must b...
The DLR Bremen with the Kryo Lab as testing facility provides the service of both static and dynamic...
DLR arc heated facility LBK with the two test legs L2K (1 MW) and L3K (6 MW) has been improved and m...
The M3 test field at DLR Lampoldshausen has been in service for research and technology development ...
This handbook sets forth criteria for the design, analysis, quality assurance, and documentation of ...
In combination with flight testing and computational fluid dynamics (CFD) schemes, ground based test...
Results of an ongoing collaboration between the engine manufacturer MTU and the German aerospace res...
Results of an ongoing collaboration between the engine manu-facturer MTU and the German aerospace re...
The Institute of Space Propulsion of the German Aerospace Center (DLR) has developed and set up a re...
The High Vacuum Test Facility STG enables an experimental investigation of thruster plumes to determ...
The paper reports the current status of a DLR Lampoldshausen project towards the design, erection, a...
The increasing interest in hypersonic transportation for both civil and military use results in an i...
New Siemens burner concepts thought to produce a more homogeneous air/fuel mix-ture and a better dis...
Within a joint research effort of Astrium and DLR, cold-gas test campaigns with subscale nozzles wer...
The objectives of this research were to build a facility that could simulate the expected fluid flow...
As part of FLPP3 tests about the stratification with liquids in very low temperature regions must b...
The DLR Bremen with the Kryo Lab as testing facility provides the service of both static and dynamic...
DLR arc heated facility LBK with the two test legs L2K (1 MW) and L3K (6 MW) has been improved and m...
The M3 test field at DLR Lampoldshausen has been in service for research and technology development ...