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A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy ([NASA technical paper] ; NASA/TP-1998-208464)

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy ([NASA technical paper] ; NASA/TP-1998-208464)
Microform図書
1998<YCA-NAS 1.60:208464>
National Diet Library
  • Author HeadingLallman, Frederick J Davidson, John B Murphy, Patr...

Control integration concept for hypersonic cruise-turn maneuvers microform / David L. Raney and Frederick J. Lallman (NASA technical paper ; 3136)

Control integration concept for hypersonic cruise-turn maneuvers microform / David L. Raney and Frederick J. Lallman (NASA technical paper ; 3136)
Microform図書
1992<YCA-NAS 1.60:3136>
National Diet Library
  • Author HeadingRaney, David L Lallman, Frederick J United States. National Aeron...

A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors microform / Kenneth H. Goodrich, Steven M. Sliwa, and Frederick J. Lallman (NASA technical paper ; 2907)

A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors microform / Kenneth H. Goodrich, Steven M. Sliwa, and Frederick J. Lallman (NASA technical paper ; 2907)
Microform図書
1989<YCA-NAS 1.60:2907>
National Diet Library
  • Author Heading...liwa, Steven M Lallman, Frederick J United States. National Aeron...

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