Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Scott D. Holland"'
Autor:
Scott D. Holland, Jeremy T. Pinier, Peter F. Covell, Bandu N. Pamadi, Jing Pei, Goetz H. Klopfer
Publikováno v:
Journal of Spacecraft and Rockets. 49:864-874
Publikováno v:
Journal of Spacecraft and Rockets. 38:828-835
An overview is provided of the experimental aerodynamics test program to ensure mission success for the autonomous flight of the Hyper-X research vehicle, a 12-ft-long, 2700-lb lifting body technology demonstrator designed to flight demonstrate for t
Publikováno v:
Journal of Spacecraft and Rockets. 38:811-819
NASA's Hyper-X research program was developed primarily to flight demonstrate a supersonic combustion ramjet engine, fully integrated with a forebody designed to tailor inlet flow conditions and a free expansion nozzle/afterbody to produce positive t
Publikováno v:
IIE Transactions. 28:155-165
The assembly of printed wiring boards (PWBs) typically involves the coordination of thousands of components and hundreds of part numbers in a job shop environment with up to 50 different processes and workstations. In this paper we present a greedy r
Publikováno v:
Operations Research. 43:219-230
In the last decade, the U.S. electronics industry has experienced a 10% annual growth rate in the assembly of printed wiring boards (PWBs). For many companies, this activity represents the most profitable component of their business with revenues in
Publikováno v:
IEEE Transactions on Engineering Management. 42:91-98
This paper describes a decision support system known as Integrated Scheduling, Inventory and Throughput Evaluation System (INSITES) designed to assist Texas Instruments in the day-to-day operations of printed wiring board (PWB) assembly at their faci
Autor:
Scott D. Holland, John N. Perkins
Publikováno v:
Journal of Aircraft. 31:610-615
The advantages and design requirements of propulsion/airtranie integration for the high Mach number flight of air-breathing vehicles have led to extensive study of the three-dimensional sidevv all-compression scramjet inlet in recent years. Inlets of
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A modern launch vehicle is by necessity an extremely integrated design. The accurate characterization of its aerodynamic characteristics is essential to determine design loads, to design flight control laws, and to establish performance. The NASA Are
Autor:
Jeremy T. Pinier, Scott D. Holland, Klopfer, Goetz, H., Peter F. Covell, Jing Pei, Bandu N. Pamadi
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
This paper presents the aerodynamic analysis and database development for the first stage separation of the Ares I A106 Crew Launch Vehicle configuration. Separate databases were created for the first stage and upper stage. Each database consists of
Autor:
J. Pahle, Charles R. McClinton, J. White, Walter C. Engelund, Randall T. Voland, Scott D. Holland
Publikováno v:
20th AIAA Advanced Measurement and Ground Testing Technology Conference.
This paper provides an overview of NASA's current focused hypersonic technology program, called the Hyper-X Program. The Hyper-X Program, a joint NASA program executed by the Langley Research Center and the Dryden Flight Research Center, is designed