| 1240 |
 Surface pressure coefficient distributions for axisymmetric forecowls at zero incidence (M sub infinity less than or equal to 1.5). |
94015 |
| 1240 |
Wave drag coefficient for axisymmetric forecowls at zero incidence (M sub infinity less than or equal to 1.5). |
94014 |
| 1240 |
NACA 1-series geometry representation for computational fluid dynamics. |
94013 |
| 1240 |
Pressure drag and lift contributions for blunted forebodies of fineness ratio 2.0 in transonic flow (M sub infinity less than or equal to 1.4). |
89033 |
| 1240 |
Axial pressure coefficient distributions for spherically blunted secant ogive forebodies of fineness ratio 1.0, 1.5 and 2.0 at zero incidence in transonic flow. |
83018 |
| 1240 |
The wave drag coefficient of spherically blunted secant ogive forebodies of fineness ratio 1.0, 1.5, and 2.0 at zero incidence in transonic flow. |
83017 |
| 1240 |
Axial pressure coefficient distributions for forebodies of fineness ratio 1.0, 1.5 and 2.0 at zero incidence in transonic flow. |
80008 |
| 1240 |
Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds. |
79004 |
| 1240 |
A method for estimating drag-rise Mach number at zero incidence of smooth or bumpy non-ducted axisymmetric bodies without or with fins. |
74013 |
| 1240 |
Upwash interference for wings in solid-liner wind tunnels using subsonic linearised-theory. |
95014 |
