Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles / J. Richard Spahr.
A wind tunnel investigation was conducted at a Mach number of 1.96 and at Reynolds numbers (based on the mean aerodynamic chord of the exposed wing) of 0.36 and 1.03 million to determine the normal forces, pitching moments, and rolling moments contributed by each wing panel of a cruciform-wing and b...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4146. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4146
|
|---|---|
| Y 3.N 21/5:6/4146 | Available Place a Hold |