Add to ORKGThe aerodynamic design of the NASA Altitude Wind Tunnel is presented in viewgraph format. The main topics covered are: analysis of a plenum evacuation system; airline definition and pressure loss code development; contraction geometry and code analysis; and design of the two stage fan. Flow characteristics such as pressure ratio, mach number distribution, adiabatic efficiency, and losses are shown
The Calibrated Ancillary System (CAS) provides real-time calibrated parameters from the orbiter down...
NASA-Langley is sponsoring a rotorcraft structural dynamics program with the objective to establish ...
The results are presented for a NASA Phase 1 study conducted from mid 1987 through mid 1989 at Ames ...
This study addresses future space applications and the derived requirements these potential applicat...
The early mission model was developed through a survey of the potential user market. Service functio...
The views of GE and P&W on the High Speed Civil Transport (HSCT) are presented in viewgraph format. ...
The intent here is to discuss the status of the boundary element method (BEM) for structural analysi...
A study was conducted to evaluate ultrasonic cleaning systems for precision cleaning effectiveness f...
The main objectives are: a model of a replicated system with exact-match voting; a fault model that ...
The transputer parallel processing lab at NASA Lewis Research Center (LeRC) consists of 69 processor...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
Conceptual design and test program for manned Mars Excursion Module /MEM/ mission in 1980 perio
Avionics is the connecting link that integrates the hardware and software which satisfy systems requ...
This report covers a portion of an ongoing investigation of the durability of titanium alloys for th...
The focus here is on one aspect of the Computational Structural Mechanics (CSM) Testbed: finite elem...
The Calibrated Ancillary System (CAS) provides real-time calibrated parameters from the orbiter down...
NASA-Langley is sponsoring a rotorcraft structural dynamics program with the objective to establish ...
The results are presented for a NASA Phase 1 study conducted from mid 1987 through mid 1989 at Ames ...
This study addresses future space applications and the derived requirements these potential applicat...
The early mission model was developed through a survey of the potential user market. Service functio...
The views of GE and P&W on the High Speed Civil Transport (HSCT) are presented in viewgraph format. ...
The intent here is to discuss the status of the boundary element method (BEM) for structural analysi...
A study was conducted to evaluate ultrasonic cleaning systems for precision cleaning effectiveness f...
The main objectives are: a model of a replicated system with exact-match voting; a fault model that ...
The transputer parallel processing lab at NASA Lewis Research Center (LeRC) consists of 69 processor...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
Conceptual design and test program for manned Mars Excursion Module /MEM/ mission in 1980 perio
Avionics is the connecting link that integrates the hardware and software which satisfy systems requ...
This report covers a portion of an ongoing investigation of the durability of titanium alloys for th...
The focus here is on one aspect of the Computational Structural Mechanics (CSM) Testbed: finite elem...
The Calibrated Ancillary System (CAS) provides real-time calibrated parameters from the orbiter down...
NASA-Langley is sponsoring a rotorcraft structural dynamics program with the objective to establish ...
The results are presented for a NASA Phase 1 study conducted from mid 1987 through mid 1989 at Ames ...