Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport
By: David E. Hahne, Louis J. Glaab.
Contributors: Glaab, Louis J.; Langley Research Center.
Series: NASA/TP ; 1999-209539; NASA technical paper -- 209539.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information; National Technical Information Service [distributor
Published: 2000
Place of publication: Hampton, Va; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Numerical analysis.; Experimentation.; Data acquisition.; Lift devices.; Leading edge flaps.; Lateral control.; Lateral stability.; Analysis (Mathematics); Performance tests.
Notes: Shipping list no.: 2000-0663-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.