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Viewing 1 to 30 of 3468
2016-09-20
Technical Paper
2016-01-2017
Devesh Kumar, Konrad Juethner, Yves Fournier
The aero engine industry is experiencing both a design renaissance and an adherence to old values in recent years. Engine manufacturers have introduced remarkable next generation capabilities by achieving thermodynamic and mechanical efficiencies and exploring novel lightweighting concepts such as the open rotor configuration [1]. At the same time, the market adheres to 50+ year-old engine concepts that have proven extremely reliable and demands continuous adaption to new applications. In either domain, it is a common problem to keep engine simulation in step with changes to design, environmental conditions, and mission data – and this applied to both actual designs and those that belong to the hypothetical design space as explored in design of experiments (DOE). We present an effective simulation process and data management (SPDM) approach that hinges on a focus on components, their generalized connections and programmatic templating.
2016-07-22
WIP Standard
AS100026B
No scope available
2016-07-22
WIP Standard
AS4877F

This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.

2016-07-22
Standard
AS3549A
SCOPE IS UNAVAILABLE.
2016-06-06
Standard
AS681K
This SAE Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady state and transient performance calculated using computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight, and dimensions computed by computer programs. This standard is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. This standard is applicable to, but not limited to the following program types: data reduction, steady-state, transient, preliminary design, study, specification, status, and parametric programs.
2016-05-17
WIP Standard
JA6268
This Aerospace Recommended Practice (ARP) was created to help industry deal with existing barriers to the successful implementation of Integrated Vehicle Health Management (IVHM) technology in the aerospace and automotive sectors. That is,given the common barriers that exist, this ARP can be applied not only to aerospace but also to the automotive, commercial and military vehicle sectors. Original Equipment Manufacturers (OEMs) in all of these sectors are heavily dependant upon a large number of component suppliers in order to design and build their products. The advent of IVHM technology has accentuated the need for improved coordination and communication between the OEM and its suppliers –to ensure that suppliers design health ready capabilities into their particular components.
2016-05-10
Standard
ARP1961A
This SAE Aerospace Recommended Practice (ARP) addresses the characteristics required for the definition, development, and acquisition of a satisfactory airframe mounted accessory gearbox (AMAG).
2016-05-04
WIP Standard
AIR1873A
This document has been declared "CANCELLED" by the E32 committee as of April 2016 and has been superseded by ARP5120. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by ARP5120. Cancelled specifications are available from SAE.
Viewing 1 to 30 of 3468

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