Theoretical and experimental study of twisted and cambered delta wings designed for a Mach number of 3.5/

Main Author: Sorrells, Russell B.
Corporate Authors: United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors: Landrum, Emma J.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, 1976
Series:NASA technical note 8247
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC