Browsing Aeronautics and Astronautics - Master's degree by Title
Now showing items 1-20 of 2245
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A 3-D tunnel correction panel method for swept tapered airfoils with separation
(Massachusetts Institute of Technology, 1988) -
3D turbine tip clearance flow redistribution due to gap variation
(Massachusetts Institute of Technology, 1991) -
Abort scenario feasibility for the manned Mars mission
(Massachusetts Institute of Technology, 1991) -
Accelerated Bayesian experimental design for chemical kinetic models
(Massachusetts Institute of Technology, 2010)The optimal selection of experimental conditions is essential in maximizing the value of data for inference and prediction, particularly in situations where experiments are time-consuming and expensive to conduct. A general ... -
Accelerated computational modeling of ballistic helmet test protocols
(Massachusetts Institute of Technology, 2017)In modern combat, helmets play a vital role in protecting the head. Before being delivered to the soldier, combat helmets undergo a series of tests to determine their threat mitigation performance. During ballistic testing, ... -
Accelerated tests of environmental degradation in composite materials
(Massachusetts Institute of Technology, 1998)High temperature polymer matrix composites are key candidates for the structural components of proposed supersonic transport aircraft. The operational environment of these vehicles exposes the airframe to harsh conditions, ... -
Accelerometer calibration of shuttle-based experiment packages
(Massachusetts Institute of Technology, 1991) -
Accurate belief state update for probabilistic constraint automata
(Massachusetts Institute of Technology, 2005)As autonomous spacecraft and other robotic systems grow increasingly complex, there is a pressing need for capabilities that more accurately monitor and diagnose system state while maintaining reactivity. Mode estimation ... -
Achieving fault tolerance via robust partitioning and N-Modular Redundancy
(Massachusetts Institute of Technology, 2007)This thesis describes the design and performance results for the P-NMR fault tolerant avionics system architecture being developed at Draper Laboratory. The two key principles of the architecture are robust software ... -
Achieving real-time mode estimation through offline compilation
(Massachusetts Institute of Technology, 2003) -
Acoustic and thermal packaging of small gas turbines for portable power
(Massachusetts Institute of Technology, 2009)To meet the increasing demand for advanced portable power units, for example for use in personal electronics and robotics, a number of studies have focused on portable small gas turbines. This research is concerned with ... -
Acoustic noise suppression for helicopter communication systems
(Massachusetts Institute of Technology, 1993) -
Acquisition and control of a precision formation flying mission
(Massachusetts Institute of Technology, 2010)Using formation flying spacecraft as space-based interferometers will provide images of unprecedented resolution. Missions such as Stellar Imager plan to use multiple spacecraft in a formation instead of a typical monolithic ... -
Acquisition strategies for commonality across complex aerospace systems-of-systems
(Massachusetts Institute of Technology, 2011)Commonality is a system architecting strategy widely used to improve affordability and reliability of families of products. However not all commonality is beneficial, and organizations must balance commonality benefits and ... -
Active control of centrifugal-compressor surge
(Massachusetts Institute of Technology, 1989) -
Active control of particulate contamination for a Leo spacecraft environment
(Massachusetts Institute of Technology, 1993) -
Active control of rotating stall in a three-stage axial compressor with jet actuators
(Massachusetts Institute of Technology, 1997) -
Active control of rotating stall in a transonic compressor stage with inlet distortion
(Massachusetts Institute of Technology, 1999)Rotating stall has been stabilized in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were conducted at the NASA Lewis Research Center on a single-stage ... -
Active control of separation induced distortion in a scaled tactial aircraft inlet
(Massachusetts Institute of Technology, 2001) -
Active control of tiltrotor blade in-plane loads during maneuvers
(Massachusetts Institute of Technology, 1988)
