Aerodynamic characteristics of a hypersonic research airplane concept having a 70o swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0/

Main Author: Penland, Jim A.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors: Hallissy, James B.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979
Series:NASA technical paper 1552
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC