Characteristics Method applied to the shock tube problem
... section of the tube, this pressure will limit the expansion wave to a narrower fan as sketched. The solution can be extended to the case where the ”right” fluid is also in motion. This then provides a numerical method called Godunov method introduced later on. The diaphragm represents the interface ...
... section of the tube, this pressure will limit the expansion wave to a narrower fan as sketched. The solution can be extended to the case where the ”right” fluid is also in motion. This then provides a numerical method called Godunov method introduced later on. The diaphragm represents the interface ...
1 - vnhsphysics
... (5) v2 = [(15 m/s)2 – 2(9.8 m/s2)(3 m)]1/2 (6) v2 = 12.9 m/s (7) Second Equation: A1v1 = A2v2 (8) A2 = A1v1 / v2 (9) A1 = r2 (10) A2 = (r2)v1 / v2 (11) A2 = (0.04 m)2(15 m/s) / (12.9 m/s) (12) A2 = 5.84 x 10-3 m2 BERNOULLI’S PRINCIPLE Bernoulli’s principle states that swiftly moving fluids exert ...
... (5) v2 = [(15 m/s)2 – 2(9.8 m/s2)(3 m)]1/2 (6) v2 = 12.9 m/s (7) Second Equation: A1v1 = A2v2 (8) A2 = A1v1 / v2 (9) A1 = r2 (10) A2 = (r2)v1 / v2 (11) A2 = (0.04 m)2(15 m/s) / (12.9 m/s) (12) A2 = 5.84 x 10-3 m2 BERNOULLI’S PRINCIPLE Bernoulli’s principle states that swiftly moving fluids exert ...
Aircraft Stability and Control AE 2350 Lecture Notes #11
... The price paid for a large static stability margin • The aircraft may become sluggish, hard to maneuver. The tail will resist the pilot’s attempt to change the aircraft “angle of attack.” • A large tail adds to aircraft weight, and cost. • A smaller tail will require a long fuselage(“ a long enough ...
... The price paid for a large static stability margin • The aircraft may become sluggish, hard to maneuver. The tail will resist the pilot’s attempt to change the aircraft “angle of attack.” • A large tail adds to aircraft weight, and cost. • A smaller tail will require a long fuselage(“ a long enough ...
