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 - discussion p 559-61; Shell Aviation News n 243 Sept 1958 p 14-18; Aeroplane v 94 n 2429 Mar 21 1958 p 396-7)
Flight tests of meteor aeroplane fitted with jet deflection
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 62 , n 572
1958
20 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Flight tests of meteor aeroplane fitted with jet deflection
Engineering Index Backfile | 1958
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