Add to ORKGPreliminary results are presented from an investigation to determine the influence of afterbody geom...
Simulated wing effect on pressure drag coefficient of subsonic boattail at angle of attac
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of ...
Jet effects on boattail axial force of conical afterbodies at subsonic and transonic speed
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
The use of external modifications in the base region to reduce the base drag of a blunt-base body in...
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersoni...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
THEproblem of wake .ow at high speeds and the drag associated with it are a signi.cant source of obs...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
The effectiveness of a trailing disk (the trapped vortex concept) in reducing the blunt base drag of...
Experiments have been carried out in the 0.5-m base flow wind tunnel at high speeds evaluating the d...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Preliminary results are presented from an investigation to determine the influence of afterbody geom...
Simulated wing effect on pressure drag coefficient of subsonic boattail at angle of attac
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of ...
Jet effects on boattail axial force of conical afterbodies at subsonic and transonic speed
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
The use of external modifications in the base region to reduce the base drag of a blunt-base body in...
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersoni...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
THEproblem of wake .ow at high speeds and the drag associated with it are a signi.cant source of obs...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
The effectiveness of a trailing disk (the trapped vortex concept) in reducing the blunt base drag of...
Experiments have been carried out in the 0.5-m base flow wind tunnel at high speeds evaluating the d...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Preliminary results are presented from an investigation to determine the influence of afterbody geom...
Simulated wing effect on pressure drag coefficient of subsonic boattail at angle of attac
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of ...