100 |
The influence of body geometry and flow conditions on axisymmetric boundary layers at subcritical Mach numbers. |
79020 |
100 |
The influence of body geometry and flow conditions on axisymmetric velocity distributions at subcritical Mach numbers. |
78037 |
100 |
Geometrical characteristics of typical bodies.
|
77028 |
100 |
Transonic drag rise of rectangular symmetrical section wings at zero lift. NACA 65 series sections. |
Aero W.S.02.03.09 |
100 |
Theoretical lift-dependent drag of wings at supersonic speeds. |
Aero W.S.02.03.02 |
100 |
Drag due to lift for non-planar swept wings up to high angles of attack at subsonic speeds. |
96025 |
100 |
Drag due to lift for plane swept wings, alone or in combination with a body, up to high angles of attack at subsonic speeds. |
95025 |
100 |
Computer program for estimation of leading-edge suction distribution for plane thin wings at subsonic speeds.
|
94038 |
100 |
Leading-edge suction distribution for plane thin wings at subsonic speeds. |
94037 |
100 |
Wave drag of wings at zero lift in inviscid airflow.
|
75004 |