Derivation of Aero-Induced Fluctuating Pressure Environments for Ares I-X

A description is given of the external aero-inducted fluctuating pressure model which was fit and anchored to wind tunnel data from the past 40 years. This model is based upon the assumption that the flow around a vehicle can be divided into discrete flow zones with independent fluctuating pressure...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Yang, Michael Y., Wilby, John F.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Spacecraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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