Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5

An edition of Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5 (1995)

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

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Publish Date

1995

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service [distributor

Language

eng

Pages

Description:

subjects: Lifting bodies, Controllability, Dihedral angle, Supersonic speed, Mach number fins, Wind tunnel tests, Deflection