A New Tyre, Brake and Undercarriage Testing Machine: Particulars of the Test Rig Designed and Built in Australia for the Testing of Individual Components or Complete Units within a Static Wheel load of 2,500–50,000 lb. and with a Maximum Overall Height of 10 feet

By Green J.R.   Wills H.A.  

Aircraft Engineering, Vol. 21, Iss. 1, 1993-12 ,pp. : 22-24

Emerald Group Publishing Ltd

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A New Approach to Fatigue Testing: A Description of the Dowty Rotol Range of Random Load Fatigue Testing Machines

By Knights R.N.  

Aircraft Engineering, Vol. 35, Iss. 7, 1993-12 ,pp. : 200-202

Emerald Group Publishing Ltd

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Testing of Advanced Carbon Fibre Wings for New Experimental Aircraft

By  

Aircraft Engineering, Vol. 58, Iss. 3, 1993-12 ,pp. : 24-24

Emerald Group Publishing Ltd

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Research and Testing

By  

Aircraft Engineering, Vol. 35, Iss. 12, 1993-12 ,pp. : 372-372

Emerald Group Publishing Ltd

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Research and Testing

By  

Aircraft Engineering, Vol. 36, Iss. 3, 1993-12 ,pp. : 85-85

Emerald Group Publishing Ltd

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