Dynamic characteristics of a KC-10 wing-pod refueling hose by numerical simulation

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Vassberg, John C ^a   Yeh, David T ^a   Blair, Andrew J ^a   Evert, Jacob M ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANTENNAS; DEGREES OF FREEDOM (MECHANICS); HOSE; VORTEX FLOW;

AERIAL REFUELING; AERODYNAMIC MODELING; COUPLING PROCESS; DYNAMIC CHARACTERISTICS; FLIGHT CONDITIONS; HORSESHOE VORTICES; LANDING CONDITIONS; SIX DEGREE-OF-FREEDOM;

NUMERICAL MODELS;

EID: 85067319213     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2712     Document Type: Conference Paper

References (4)

1. KC-10 Flight Manual TO 1-1C-1-33, loss of wing pod drogue
2. Vassberg, John and Prescott, Chuck; "Static and Dynamic Simulations of the KC-10 Hose," KC-10 Centerline Hose Reel Improvements Workshop, April 1993, Tinker Air Force Base
3. Allen, John, communication re: wing pod strake development wind tunnel program
4. MIL-H-4495D, "Hose Assembly, Rubber, Aerial Refueling," 10 May, 1985