Opening book details…
About this book
Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability by Taylor, John G. is a book available to read on EtoBox.
- Author
- Taylor, John G.
- Publisher
- National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990.
- Published
- 1990
- Language
- EN
More by Taylor, John G.
Browse all works by Taylor, John G.
Similar books
- Static Performance of an Axisymmetric Nozzle with Post-exit Vanes for Multiaxis Thrust Vectoring / Bobby L. Berrier and Mary L. Mason. — Bobby L. Berrier (1988)
- CFD Modelling of the Coanda Based Thrust Vectoring Nozzle — A. Suñol; D. Vucinic; S. Vanlanduit (2014)
- An Experimental Investigation of Thrust Vectoring Two-dimensional Covergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack / Francis J. Capone, Mary L. Mason, and Laurence D. Leavitt. — Francis J. Capone (1990)
- Characteristics Of A Confined Jet Thrust Vector Control Nozzle (1985)
- Reconfigurable Two‐Dimensional DNA Lattices: Static and Dynamic Angle Control
- Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability / Linda S. Bangert and Laurence D. Leavitt. — Linda S. Bangert (1989)