In combination with flight testing and computational fluid dynamics (CFD) schemes, ground based testing is a mandatory tool to be used in the design and development process of future air breathing propulsion systems. In fact it is the optimised combination of all three tools which is required to advance the knowledge in this field and to develop the database necessary for the development of operational highly integrated vehicles. In the present paper, the operational German ground based test capabilities for high speed air breathing propulsion are summarised. This overview is restricted to test facilities which allow testing including combustion and cold hypersonic tunnels which are used for intake, nozzle and fuel off combustor testing are...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
The present interim report summarizes all activities carried out since the beginning of the ''Propul...
Ground based testing of a supersonic combustion ramjet (scramjet) configuration used in the framewor...
Successful research and development of hypersonic vehicles require an integrated test and evaluation...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
During the past years extensive work on an airbreathing propulsion system for a hypersonic applicati...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
Flying at hypersonic Machnumbers using airbreathing propulsion requires highly sophisticated design ...
In the framework of the European Commission co-funded LAPCAT (Long-Term Advanced Propulsion Concepts...
From the very beginning the DLR Institute of Space Propulsion in Lampoldshausen has been involved in...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) is one of the ma...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) is one of the ma...
The high speed flows with mach number above 5 are generally categorised as hypersonic flows. In orde...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
The present interim report summarizes all activities carried out since the beginning of the ''Propul...
Ground based testing of a supersonic combustion ramjet (scramjet) configuration used in the framewor...
Successful research and development of hypersonic vehicles require an integrated test and evaluation...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
During the past years extensive work on an airbreathing propulsion system for a hypersonic applicati...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
Flying at hypersonic Machnumbers using airbreathing propulsion requires highly sophisticated design ...
In the framework of the European Commission co-funded LAPCAT (Long-Term Advanced Propulsion Concepts...
From the very beginning the DLR Institute of Space Propulsion in Lampoldshausen has been involved in...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) is one of the ma...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) is one of the ma...
The high speed flows with mach number above 5 are generally categorised as hypersonic flows. In orde...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
The present interim report summarizes all activities carried out since the beginning of the ''Propul...
Ground based testing of a supersonic combustion ramjet (scramjet) configuration used in the framewor...