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ARC / R&M 3535
Eldridge,R H
       A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW / .- Her Majesty'S Stationery Office, London, 1968 .- 49 .
Bound With Arc R&M3533,3542-49 Lack No.3534,3536-41,3547
Author Added Entry:
Walkden,F;
Copy Details:
Acc. No.: TR17086, Full Call No.: ARC R&M 3535, Item type: Technical Report , Location: General Stacks,
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