Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
By: Christopher I. Cruz and George M. Ware.
Contributors: Ware, George M.; Langley Research Center.
Series: NASA technical memorandum -- 4697.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service [distributor
Published: 1995
Place of publication: Hampton, Va; Linthicum Heights, MD; NASA Center for AeroSpace Information [distributor]; Springfield, VA
Language: eng
Format: Microform
Subjects: Controllability.; Deflection.; Dihedral angle.; Lifting bodies.; Mach number fins.; Supersonic speed.; Wind tunnel tests.
Other titles: Control effectiveness and tip fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0466-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.