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- W327213414 abstract "From Summary: The results of numerous unrelated tests of dive-recovery flaps are collected in this report and presented in a form suitable for use in the preliminary design of dive-recovery flap installations. Since the data were obtained for airplane models of quite widely varying configurations, and are limited largely to a Mach number of 0.80, it is recommended that each new installation be carefully flight-tested before final approval. A flight-test procedure is outlined which will insure a maximum degree of safety." @default.
- W327213414 created "2016-06-24" @default.
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- W327213414 date "1947-09-09" @default.
- W327213414 modified "2023-09-27" @default.
- W327213414 title "A summary and analysis of data on dive-recovery flaps" @default.
- W327213414 hasPublicationYear "1947" @default.
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