1. n 294 p 14-16: Paper reports on work done at RAE, Farnborough, and British aircraft firms on some specifically aerodynamic problems; attempt is made to explain dominant and typical aerodynamic problems and how these can be solved; paper is restricted to slender wings of predominantly light-alloy construction with turbojet engines, to cruise at about twice speed of sound. 2. n 295 p 14-19: Design of volume distribution, and limitations and boundaries to flight regime; diagrams.
Slender wings for supersonic flight
Shell Aviation News
Shell Aviation News ; n 294-295
1962
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Swept wings in supersonic flight
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