Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 /
E. Ann Bare and David E. Reubush, Raymond C. Haddad.
Description
| Main Author: | Bare, E. Ann. |
|---|---|
| Related Names: | Haddad, Raymond C. , Reubush, David E. |
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992. |
| Subjects: |
Fighter planes.
Flaps (Airplanes) Leading edges (Aerodynamics) Airplanes > Airplanes / Control systems. Airplanes > Airplanes / Wings, Triangular. Vortex-motion. |
| Note: |
Prepared at Langley Research Center. |
| Physical Description: |
iv, 121 p. :
ill. ;
28 cm.
|
| Locate a Print Version: |
Find in a library |
Viewability
| Item Link | Original Source |
|---|---|
| Full view | University of Illinois at Urbana-Champaign |