2 edition of calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow found in the catalog.
calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow
Jeremy H. B. Smith
|Statement||by J. H. B. Smith [and others].|
|Series||Aeronautical Research Council. Reports and memoranda,, no. 3471, Reports and memoranda (Aeronautical Research Council (Great Britain)) ;, no. 3471.|
|LC Classifications||TL526.G7 A4 no. 3471|
|The Physical Object|
|Number of Pages||36|
|LC Control Number||67108712|
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