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- 71855084%2F%2Fr862 contributor B2052974.
- 71855084%2F%2Fr862 created "1969.".
- 71855084%2F%2Fr862 date "1969".
- 71855084%2F%2Fr862 date "1969.".
- 71855084%2F%2Fr862 dateCopyrighted "1969.".
- 71855084%2F%2Fr862 description "Includes bibliographical references.".
- 71855084%2F%2Fr862 extent "12, [18] p.".
- 71855084%2F%2Fr862 identifier "0114701865".
- 71855084%2F%2Fr862 isPartOf "Aeronautical Research Council. Current papers, no. 1059".
- 71855084%2F%2Fr862 isPartOf "Current papers (Aeronautical Research Council (Great Britain)) ; no. 1059.".
- 71855084%2F%2Fr862 issued "1969".
- 71855084%2F%2Fr862 issued "1969.".
- 71855084%2F%2Fr862 language "eng".
- 71855084%2F%2Fr862 publisher "London, H.M. Stationery Off.,".
- 71855084%2F%2Fr862 subject "629.13/008 s".
- 71855084%2F%2Fr862 subject "Airplanes Nacelles.".
- 71855084%2F%2Fr862 subject "Airplanes Wings.".
- 71855084%2F%2Fr862 subject "Boundary layer.".
- 71855084%2F%2Fr862 subject "TL507 .G77 no. 1059 TL681.5".
- 71855084%2F%2Fr862 subject "Wind tunnels.".
- 71855084%2F%2Fr862 title "Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing, by R. T. Griffiths.".
- 71855084%2F%2Fr862 type "text".