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Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing
Language: en
Pages: 1
Authors: JOHN W. PAULSON
Categories:
Type: BOOK - Published: 1961 - Publisher:

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A model was flown over an angle-of-attack range from 10 to 35 degrees. Longitudinal stability and control characteristics were generally satisfactory with neutr
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78° Delta Wing
Language: en
Pages: 31
Investigation of the Low Subsonic Flight Characteristics of a Model of a Flat-top Hypersonic-boost Glide Configuration Having an Arrowhead Wing
Language: en
Pages: 26