A method for obtaining practical flutter-suppression control laws using results of optimal control theory/
Main Author: | Newsom, Jerry R. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Branch ,
1979
|
Series: | NASA technical paper
1471 |
Subjects: |
Similar Items
-
Effect of cage design on characteristics of high-speed-jet-lubricated 35-millimeter-bore ball bearing/
by: Schuller, Fredrick T.
Published: (1980) -
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients/
by: Sanders, Bobby W.
Published: (1980) -
Guide to in-flight thrust measurement of turbojets and fan engines/
Published: (1979) -
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet/
by: Sanders, Bobby W.
Published: (1980) -
Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude/
by: Straight, David M.
Published: (1983)