HMSO-R&M-995 / -
Turner,K. J., Ross,A. Jean
       DYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4 / .- Her Majesty'S Stationery Office, London, 1968 .- 67 .
Bound With Hmso-R&M-991-99
Author Added Entry:
Earley,Geraldine;
Copy Details:
Acc. No.: TR9652, Full Call No.: HMSO-R&M-995 -, Item type: Technical Report , Location: General Stacks,
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