Systematic study of projectile aerodynamics made in spark photography range of Ballistic Research Laboratory, and results on drag are sufficiently complete to have general application to compressible flow problems; application made of these ballistic results to design of supersonic aircraft fuselage shape giving minimum drag, with fixed body diameter and with arbitrary choice of conical head and boattail. (See also - n 3 (letter to editor) Sept p 519)
Some ballistic contributions to aerodynamics
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 14 , n 3
1947
12 pages
Article (Journal)
English
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Aerodynamics of the EXPERT Re-Entry Ballistic Vehicle
British Library Conference Proceedings | 2009
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