Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers/

Main Author: Blair, A. B.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors: Allen, Jerry M., Hernandez, Gloria
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983
Series:NASA technical paper 2157
Subjects:
Physical Description:83 σ. : εικ. ; 28 εκ.
Bibliography:Περιέχει βιβλιογραφικές παραπομπές