Add to ORKGAn investigation has been made in the Langley 9- by 12-inch super-sonic blowdown tunnel at Mach numbers of 1.62 and 1.96 of a partial-span body with one tail surface, designed for use on the Hughes Falcon (MX-904) missile. The present paper extends the work reported in NACA-RM-SL50E10. Force and moment data including elevator hinge moment were obtained for the conditions of the tail in the presence of a small segment of the fore-shortened body, in the presence of a semi-span body and attached to a semi-span body, and for the condition of the foreshortened semi-span body alone
A wind tunnel investigation has been conducted to determine the longitudinal and lateral aerodynamic...
A parametric study of wrap-around-fin missile configurations has been conducted at Mach numbers from...
The results of the investigation indicated that, for tails having subsonic leading edges and superso...
An investigation has been made in the Langley 9- by 12-inch super-sonic blowdown tunnel at Mach numb...
An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing...
The static longitudinal stability characteristics of a 0.15-scale model of the Hermes A-lE2 missile ...
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing a...
An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine th...
At the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterroch...
"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet
An investigation has been made in the Langley 4- by 4-foot super-sonic pressure tunnel to determine ...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
Time histories of rolling and yswing moments on incl-ined bodies of revolution with vertical-tail su...
An investigation of the characteristics of a wing with an aspect ratio of 9.0 and an NACA 65-210 air...
In this paper, the rst experimental results of tests with a new model support designed for simulatio...
A wind tunnel investigation has been conducted to determine the longitudinal and lateral aerodynamic...
A parametric study of wrap-around-fin missile configurations has been conducted at Mach numbers from...
The results of the investigation indicated that, for tails having subsonic leading edges and superso...
An investigation has been made in the Langley 9- by 12-inch super-sonic blowdown tunnel at Mach numb...
An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing...
The static longitudinal stability characteristics of a 0.15-scale model of the Hermes A-lE2 missile ...
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing a...
An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine th...
At the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterroch...
"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet
An investigation has been made in the Langley 4- by 4-foot super-sonic pressure tunnel to determine ...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
Time histories of rolling and yswing moments on incl-ined bodies of revolution with vertical-tail su...
An investigation of the characteristics of a wing with an aspect ratio of 9.0 and an NACA 65-210 air...
In this paper, the rst experimental results of tests with a new model support designed for simulatio...
A wind tunnel investigation has been conducted to determine the longitudinal and lateral aerodynamic...
A parametric study of wrap-around-fin missile configurations has been conducted at Mach numbers from...
The results of the investigation indicated that, for tails having subsonic leading edges and superso...