Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63/

Main Author: Pittman, Jimmy L.
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: Riebe, Gregory D.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:NASA technical paper 1767
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC