Gloster Meteor RA.490 used as test aircraft; all aerodynamic tests made on model giving nominal deflection angle of 70°; performance measurements on flight deflectors; qualitative handling tests; lift, drag and thrust measurements; flight experiment showed that stability and control of Meteor were adequate for test flying at speeds down to 70% of normal stalling speed. (See also Roy Aeronautical Soc -- J v 62 n 572 Aug 1958 p 539-58 (discussion) 559-61; Shell Aviation News n 243 Sept 1958 p 14-18)
Flight tests of meteor aeroplane fitted with jet deflection
Aeroplane
Aeroplane ; 94 , n 2429
1958
2 pages
Aufsatz (Zeitschrift)
Englisch
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Flight tests of meteor aeroplane fitted with jet deflection
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