Mutual Aerodynamic Interference Effects for Multiple Bodies by the Cross-Flow Corrections Method.
Final rept. 15 Jun-15 Sep 70,
AIR FORCE ARMAMENT LAB EGLIN AFB FLA
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The complexity of the flow field beneath an aircraft with external stores is examined analytically. Equations are produced for computing store separation trajectories, based on mutual interference flow fields between the aircraft and the store. The circle theorem and the small disturbances theory are used in establishing the perturbations responsible for the flow field interference. Author
- Fluid Mechanics