Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 ̊to 110
Sue B. Grafton and Charles E. Libbey.
Description
| Main Author: | Grafton, Sue B. |
|---|---|
| Related Names: | Libbey, Charles E. |
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration ; 1971. |
| Subjects: |
Fighter planes
>
Fighter planes /
Aerodynamics.
Spin (Aerodynamics) Angle of attack (Aerodynamics) Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Aerodynamics. |
| Physical Description: |
36 p. :
ill. ;
27 cm.
|
| Locate a Print Version: |
Find in a library |
Viewability
| Item Link | Original Source |
|---|---|
| Full view | University of Illinois at Urbana-Champaign |