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- 77456512%2F%2Fr892 contributor B3134529.
- 77456512%2F%2Fr892 contributor B3134530.
- 77456512%2F%2Fr892 created "1968.".
- 77456512%2F%2Fr892 date "1968".
- 77456512%2F%2Fr892 date "1968.".
- 77456512%2F%2Fr892 dateCopyrighted "1968.".
- 77456512%2F%2Fr892 description "Bibliography: p. 21.".
- 77456512%2F%2Fr892 extent "[1], 49 p.".
- 77456512%2F%2Fr892 isPartOf "Aeronautical Research Council. Reports and memoranda, no. 3535".
- 77456512%2F%2Fr892 isPartOf "Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3535.".
- 77456512%2F%2Fr892 issued "1968".
- 77456512%2F%2Fr892 issued "1968.".
- 77456512%2F%2Fr892 language "eng".
- 77456512%2F%2Fr892 publisher "London, H.M.S.O.,".
- 77456512%2F%2Fr892 subject "629.13/008 s".
- 77456512%2F%2Fr892 subject "Aerodynamics, Supersonic.".
- 77456512%2F%2Fr892 subject "Airplanes Wings.".
- 77456512%2F%2Fr892 subject "TL526.G7 A4 no. 3535".
- 77456512%2F%2Fr892 title "A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow, by R. H. Eldridge and F. Walkden.".
- 77456512%2F%2Fr892 type "text".