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612-822-4611
Integrated Conceptual Design of Joined-Wing Sensorcraft Using Response Surface Models

Integrated Conceptual Design of Joined-Wing Sensorcraft Using Response Surface Models

Paperback

Technology & EngineeringGeneral Education

ISBN10: 1288305869
ISBN13: 9781288305865
Publisher: Biblioscholar
Published: Nov 16 2012
Pages: 168
Weight: 0.54
Height: 0.36 Width: 6.14 Depth: 9.21
Language: English
A multidisciplinary conceptual design and analysis of Boeing's joined-wing SensorCraft has been conducted. This analysis was completed using geometrical optimization, aerodynamic analyses, and response surface methodology on a composite structural model. Phoenix Integration's Model Center was used to integrate the sizing and analysis codes found in Raymer's text, Aircraft Design: A Conceptual Approach as well as those from the NASA derived conceptual design tool AirCraft Synthesis (ACSYNT), and a modified Boeing Finite Element Model (FEM). This research demonstrated the utility of integrated low-order models for fast and inexpensive conceptual modeling of unconventional aircraft designs.

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