Zobrazeno 1 - 10
of 19
pro vyhledávání: '"C. Frederic Smith"'
Publikováno v:
Journal of Aircraft. 59:47-57
Aircraft-mounted gas turbine engines may need to employ a variety of inlet ducts to perform various missions. An inertial particle separator (IPS) is a type of inlet duct that can remove harmful du...
Publikováno v:
Powder Technology. 363:275-285
Natural particles, such as sand and dust, often have irregular, angular shapes without porosity. Such sedimentary particles can have a significantly different drag coefficients than spherical particles, and a robust drag coefficient model is needed t
Publikováno v:
Powder Technology. 413:118004
Publikováno v:
Journal of the American Helicopter Society. 64:1-12
An inertial particle separator (IPS) is a particulate removal device typically installed at the inlet of a gas turbine to mitigate effects of sand ingestion on the engine. This system can minimize particulate ingestion during helicopter landings in a
Publikováno v:
Measurement Science and Technology.
Publikováno v:
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
Publikováno v:
Journal of Aircraft. 33:463-469
Autor:
C. Frederic Smith
Publikováno v:
12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
I. Background The author has observed that many engineers who use optimization related software do not have formal training in this discipline. Based on interaction with users the author considers optimization still a niche discipline that is gaining
Autor:
C. Frederic Smith
Publikováno v:
13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference.
The application of Six Sigma design methods to an inlet particle separator is presented in this paper. As stated in the book “Design for Six Sigma Memory Jogger” Six Sigma is a collection of methods that guides “developing new processes, produc
Autor:
C. Frederic Smith
Publikováno v:
12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
The aerodynamic design of turbofan and turboshaft engine exhaust systems can be a very iterative process. There are several key parameters to consider for the design of a high performance exhaust system for aerospace applications. The design of these