Stanford undergraduates may declare a Major in Aeronautics and Astronautics leading to the Bachelor of Science in. See list of Approved Courses in Undergraduate Engineering Handbook website at ughb.stanford.edu, Figure 4-4: 3-5: Aero/Astro Depth Requirements 27 units minimum ENGR 14: Intro to Solid Mechanics (required) 3: ENGR 15: Dynamics. Composites Engineering Handbook by P. Mallick, 043, available at Book Depository with free delivery worldwide.

Element 6 Composites - Technical:: Composite Materials • • • • • • • • • • • • • • • • • • • • • • Composite Materials Many different types of materials are used to create composites. Below is a description of the most commonly used at Element 6 Composites. Honeycomb • Polypropylene Honeycomb: The advantages of the polypropylene honeycomb is that it is tough and durable, resulting in a strong impact resistant laminate.

Additional properties also include resistance to moisture, and high sound and vibration attenuation. • Aramid (Nomex) Honeycomb: Aramid fiber paper (for example, Nomex from DuPont Corporation) is an excellent lightweight non-metallic core material.

Nomex offers excellent resiliency, low density, corrosion resistance, flame retardancy, and good compressive strength to weight ratio. Brs Pencil Tool Plugin. • Kevlar Honeycomb: Like Nomex, Kevlar from DuPont Corporation is also manufactured from aramid fibers. However, the structural properties of Kevlar are better than Nomex, particularly in compressive strength. • Carbon-Fiber Honeycomb: Carbon-fiber can also be used as a core material; however, the cost is very high. Structures with this type of construction are often limited to space applications, for example, satellites, where weight savings is critical, and the thermal expansion needs to be kept at a minimum. Pink Panther Passport To Peril Free Download Mac there.

• Metal Honeycomb: Various metal honeycomb core materials are available, depending on the application. Aluminum is a common metal used for honeycomb cores, particularly when used with fiberglass face sheets. The compressive and shear strength of aluminum honeycomb are excellent. Foams Foam cores produce extremely lightweight composite structures. Many different types of foams are available, depending on the application.

In addition, foam volumetric density can range from as low as 1.0 lbs/ft3 to over 60 lbs/ft3. High density foam cores provide greater resistance to compression and crush, as well as provide damage tolerance from impact. Low density foam cores with carbon-fiber face sheets, particularly in thicknesses greater 1”, can produce panels with extraordinarily high stiffness to weight ratio. A few examples of foams cores commonly used in composite structures at Element 6 Composites are: • Airex Foam Core: Airex is a closed cell, cross-linked polymer foam, which is lightweight and has good impact strength. • Depron Foam Core: Depron is an inexpensive, non-structural foam.

A Depron carbon fiber foam core laminate has excellent strength and stiffness in bending; however, lacks the compressive strength and crushing resistance of a structural foam core. • Divinycell Foam Core: Divinycell foam core is a medium density structural foam with very high strength, often used for heavier duty applications where lighter density foams may not work.

In particular, Divinycell H100 is an excellent damage tolerant foam, and is ideal for applications that require resistance to impact and local crushing. Wood • Balsa Wood: Balsa wood, when used as a core material in composite fabrication, offers a very high strength and stiffness to weight ratio.

End grain balsa provides exceptionally high shear, tensile and compressive strengths for its weight. Balsa is also a renewable resource, with typical balsa trees maturing to 90 feet in seven years. • Birch Plywood: Birch plywood is higher density than balsa wood, providing a durable final product with excellent compressive strength, resistance to local crushing, and machinability. Do You Have a Project? Manufacturing Need? 315.252.2559 Monday-Friday 9:00am-5:00pm ET.