29th AIAA Applied Aerodynamics Conference 2011
DOI: 10.2514/6.2011-3504
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Overview of Orion Crew Module and Launch Abort Vehicle Dynamic Stability (Invited)

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Cited by 24 publications
(11 citation statements)
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“…This technique was matured during the Apollo program and is still in use today. It allows for explicit determination of the reduced frequency inherent to the vehicle (as opposed to sweeping through various possibilities as in forced oscillation technique) [20], is simple in its implementation, and requires only one measurement (oscillation amplitude as a function of time) [13]. Similar to the forced oscillation setup, free oscillation testing yields an average value of the damping over one oscillation cycle and suffers from the effects of having a sting present to modify the wake flow.…”
Section: B Free Oscillation Testingmentioning
confidence: 99%
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“…This technique was matured during the Apollo program and is still in use today. It allows for explicit determination of the reduced frequency inherent to the vehicle (as opposed to sweeping through various possibilities as in forced oscillation technique) [20], is simple in its implementation, and requires only one measurement (oscillation amplitude as a function of time) [13]. Similar to the forced oscillation setup, free oscillation testing yields an average value of the damping over one oscillation cycle and suffers from the effects of having a sting present to modify the wake flow.…”
Section: B Free Oscillation Testingmentioning
confidence: 99%
“…In order to capture the dynamic behavior, a motor attached to the sting imparts a one-degree-offreedom oscillatory motion to the vehicle at a wide range of frequencies and mode shapes. Sinusoidal motion is typically used [20]. The vehicle is inclined at a wide range of angles of attack and at each condition undergoes a series of small amplitude pitch oscillations.…”
Section: A Forced Oscillation Testingmentioning
confidence: 99%
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