Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude/

Main Author: Straight, David M.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, Lewis Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Branch
Other Authors: Cullom, Richard R.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration Scieentific and Technical Information Branch, 1983
Series:NASA technical paper 2171
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC