Jarrett K. Huffman

Hinged strakes for enhanced maneuverability at high angles of attack

Dhanvada M. Rao, Jarrett K. Huffman, 1981 .

Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration. [Langley 7- by 10-ft high speed tunnel tests

C. H. Fox, Charles H. Fox, R. L. Campbell, 1983 .

Subsonic longitudinal aerodynamic characteristics and engine pressure distributions for an aircraft with an integrated scramjet designed for Mach 6 cruise. [conducted in Langley 7 by 10 foot high speed tunnel

C. H. Fox, P. J. Johnston, Jarrett K. Huffman, 1977 .

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

Charles H. Fox, Sheryll Goecke Powers, Jarrett K. Huffman, 1986 .

Leading-edge deflection optimization for a highly swept arrow wing configuration

James W. Fenbert, Paul L. Coe, Jarrett K. Huffman, 1980 .