Aerospace

What we do

What’s new?

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A new defensive pod technology for fast jets

LThe CS IR has assisted local small business Sysdel CC with integrating its new pod with a South African Air Force aircraft. The Acepod store integration is an example of how the CSIR supports local SMMEs to grow into world-class aerospace enterprises that can compete globally to the national benefit.

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Extraction process

Moving to green aviation: Hydrogen fuel cell technology demonstrated

For the first time in South Africa, CSIR researchers have demonstrated hydrogen fuel cell propulsion suitable for unmanned aerial vehicles (UAVs). The demonstration was conducted using a hybrid fixed-wing, vertical take-off and landing UAV in a hardware-in-the-loop setup. While the hydrogen fuel cell research is still in its early development stages, once completed, a commercially viable fuel cell propulsion system will be licensed to a local partner for industrialisation and commercialisation.

Our Research

Experimental aerodynamics
Experimental aerodynamics

Central to our experimental aerodynamics work is a suite of wind tunnels, covering a range from low-subsonic to supersonic speeds, along with associated analytical tools and models. We have developed unique aeroelasticity test rigs and technologies, including ground vibration testing tools for light aircraft and in-flight excitation systems for flutter flight testing of aircraft ranging from light to supersonic.

Platform design
Platform design

We undertake conceptual and detailed design, as well as aerodynamic characterisation of fixed- and rotary-winged aircraft. This is achieved through wind tunnel testing and computational methods such as high-fidelity, man-in-the-loop simulations. Design examples include gyrocopters, UAVs, light aircraft and gas turbine engines.

Propulsion
Propulsion

Our core capabilities in propulsion include cycle modelling, efficiency enhancement and life extension of turbines, supported by a range of specialised infrastructure. Beyond gas turbines or turbojet engines, our focus extends to new energy sources.

Aircraft store integration
Aircraft store integration

We have expert knowledge in evaluating the aerodynamic and mechanical impacts of integrating stores with aircraft. Our work includes aeroelasticity (flutter), store separation behaviour and the loads imposed on aircraft during carriage, as well as the impact on aircraft performance and handling characteristics. CSIR-developed tools, codes and testing facilities are used for store separation analysis.

Flight test support
Flight test support

We provide support for the entire test programme, including flight set specification design, oversight of flight execution and processing of flight test data.

Contact information:

Biko Managa
Impact Area Manager
@email

Bhavya Vallabh
Business Development Manager
@email

 

Our facilities

Vuyani Jarana
The low-speed wind tunnel

The low-speed wind tunnel is a continuous, single-return tunnel with a closed test section. Strut-mounted models are suspended from an overhead six-component virtual-centre balance. An auxiliary pitch sector allows sting-supported models to be mounted on a variety of internal strain gauge balances.

Nomsa Dlamini
The high-speed wind tunnel

The high-speed wind tunnel is a trisonic, blowdown tunnel equipped with a colour Schlieren system for flow visualisation. Subsonic and supersonic Mach numbers are tested using the standard wind tunnel setup, while transonic tests make use of an additional cart fitted with a plenum evacuation system and porous walls.

Fabrizio Dionisio
The medium-speed wind tunnel

The medium-speed wind tunnel is one of the best-equipped and most sophisticated tunnels of its kind in the southern hemisphere. It is powered by a 20 MW electric motor that drives a three-stage axial compressor with variable guide vanes and stator blade angles for accurate Mach number control. This variable-density transonic tunnel operates continuously to ensure optimum productivity and accuracy. The square test section is slotted, with a porosity of 5% to deliver the best possible flow quality at transonic Mach numbers.

Fabrizio Dionisio
The seven-metre wind tunnel

The seven-metre wind tunnel is a continuous, open-circuit tunnel powered by 28 axial-flow fans, each rated 30 kW. Uniform flow distribution across the tunnel's speed range is achieved by operating the fans in one of 13 symmetrical patterns.

Resources  

Aerospace research, development and services at the CSIR

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