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; Aeroplane v 94 n 2429 Mar 21 1958 p 396-7)
Flight tests of meteor aeroplane fitted with jet deflection
Shell Aviation News
Shell Aviation News ; 62 , n 243
1958
5 pages
Article (Journal)
English
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Flight tests of meteor aeroplane fitted with jet deflection
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