Experimental validation of the wing dihedral effect using a whirling arm equipment

Journal of Aircraft

Volumn 38, Issue 6, 2001, Pages 1069-1075

  Gili, P A ^a   Battipede, M ^a  

^a POLITECNICO DI TORINO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; NUMERICAL ANALYSIS; REYNOLDS NUMBER; ROTATION; VORTEX SHEDDING; WAKES; WINGS;

DIHEDRAL EFFECT; WHIRLING ARMS;

AERODYNAMICS;

EID: 0035516616     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2874     Document Type: Article

References (26)

1. SDNM pitch and Yaw axis stability derivatives
2. Low-speed unsteady aerodynamics of a pitching straked wing at high incidence - Part I: Test program
3. Low-speed unsteady aerodynamics of a pitching straked wing at high incidence - Part II: Harmonic analysis
4. Applications of half-model technique in dynamic stability testing
5. Direct derivative measurements in the presence of sting plunging
6. Frequency effects on dynamic stability derivatives obtained from small-amplitude oscillatory testing
7. New rotary rig at RAE and experiments on HIRM
8. Dynamic support interference in high-alpha testing
9. Reflection regarding recent rotary rig results
10. Another look at high-alpha support interference in rotary tests
11. Wind-tunnel aerodynamics in rotary tests of combat aircraft models
12. Implications of recent rotary rig results for flight prediction
13. Using oscillatory conning experimental rig for separation of rotary and unsteady aerodynamic derivatives
14. Lateral oscillations of sting-mounted models at high alpha
15. Measurements of aerodynamic rotary stability derivatives using a whirling arm facility
16. The sweep-back angle and the aerodynamic induction like wing contributions to the dihedral effect
17. Dihedral effect for straight tapered and twisted wings
18. l(β) evaluation
19. Determination of the characteristics of tapered wings
20. A generalized lifting line theory for curved and swept wings
21. Theoretical span load distributions and rolling moments for side-slipping wings of arbitrary planform in incompressible flow
22. Theory for computing span loads and stability derivatives due to sideslip, yawing and rolling for wings in subsonic compressible flow
23. v (rolling moment due to sideslip)
24. A generalized vortex lattice method for subsonic and supersonic flow applications