Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds/

Main Author: Stallings, Robert L.
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 Office, Langley Research Center
Other Authors: Lamb, Milton, Watson, Carolyn B.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980
Series:NASA technical paper 1683
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC