Tail assemblies

Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles

Mark C. Frassinelli and George T. Carson.

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

Ira J. Walker, Peter F. Covell And Dana K. Forrest.

Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters

Cynthia A. Crowell and Henry L. Kelley.

Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane

H. Paul Stough, James M. Patton and Steven M. Sliwa.

Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes

James S. Bowman, Jr., Randy S. Hultberg, Colin A. Martin.

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

Scott P. Fears, Holly M. Ross, and Thomas M. Moul.

Tailless aircraft performance improvements

Irving L. Ashkenas and David H. Klyde.

Numerical simulation of the SOFIA flowfield

Stephen P. Klotz.

Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds

William P. Henderson and James R. Burley II.

Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model

Stacey J. Cotton and Lisa J. Bjarke.