120 |
The pressure distribution at zero incidence over selected families of blunt axisymmetric forebodies. |
82018 |
120 |
Supersonic base and boat-tail pressure drag of cylindrical bodies with a conical boat-tail and a central propulsive jet
|
00017 |
120 |
Supersonic base drag of cylindrical bodies with a central propulsive jet.
|
99010 |
120 |
Effect of stabilising fins on base drag of cylindrical bodies at supersonic speeds.
|
97022 |
120 |
Effect of angle of attack on the base axial force and drag of cylindrical bodies with conical boat-tails.
|
96033 |
120 |
Supersonic pressure drag of conical, circular-arc and parabolic boat-tails.
|
00026 |
120 |
Subsonic and transonic base and boat-tail pressure drag of cylindrical bodies with circular-arc boat-tails. |
96012 |
120 |
Pressure drag of spherically-blunted conical forebodies at zero incidence for Mach numbers of 3 and above. |
82028 |
120 |
Pressure drag of blunt forebodies at zero incidence for Mach numbers up to 10.
|
80021 |
120 |
Drag increment due to rear fuselage upsweep.
|
80006 |