| 130 |
 Body effect on wing angle of attack and pitching moment at zero lift at low speeds.
|
89042 |
| 130 |
Aerodynamic centre of wing-fuselage-nacelle combinations: effect of rear-fuselage pylon-mounted nacelles. |
78013 |
| 130 |
Aerodynamic centre of wing-fuselage-nacelle combinations: effect of wing-pylon mounted nacelles.
|
77012 |
| 130 |
Aerodynamic centre of wing-fuselage combinations.
|
76015 |
| 130 |
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
|
AERO B.S.05.03.01 |
| 130 |
Supersonic pressure and Mach number distributions over conical, circular-arc and parabolic boat-tails.
|
00028 |
| 130 |
Computer program for the calculation of normal force and pitching moment of forebody-cylinder combinations at angles of attack up to 90 degrees and Mach numbers up to 5, including the effects of conical boat-tailing.
|
90034 |
| 130 |
Normal force, pitching moment and side force of forebody-cylinder combinations for angles of attack up to 90 degrees and Mach numbers up to 5.
|
89014 |
| 130 |
Normal-force-curve and pitching-moment-curve slopes of forebody-cylinder combinations at zero angle of attack for Mach numbers up to 5.
|
89008 |
| 130 |
Normal force and pitching moment of conical boat-tails. |
87033 |
