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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Analysis and flight data for a drone aircraft with active flutter suppression
(Previously cited in issue 12, p. 1935, Accession no. A81-29495)
Airplane model structure determination from flight data
Previously cited in issue 21, p. 3626, Accession no. A81-44562
Assessing the orbiter thermal environment using flight data
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Comparison of inviscid flow computations with flight data for the Shuttle orbiter
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Applications of state estimation in aircraft flight-data analysis
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Analysis of windshear from airline flight data
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Real-time comparison of X-29A flight data and simulation data
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Partitioning of flight data for aerodynamic modeling of aircraft at high angles of attack
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Low-frequency spectral representation of Space Shuttle flight data
The present digital processing of 18 accelerograms associated with Space Shuttle liftoffs splits each of the accelerograms into three time-slices, respectively representing (1) SSME thrust buildup, (2) the period immediately following the SRBs' ignition, and (3) the subsequent period of intense acoustical activity due to the exhaust plume's interactions with the launch pad. The spectral treatment of these data involve the use of autoregressive and autoregressive-moving-average filters that furnish analytical representations of the spectra for all three time-slices in terms of a set of coefficients; these coefficients are applicable to the synthesis of artificial acceleration time-histories.
Requirements analysis notebook for the flight data systems definition in the Real-Time Systems Engineering Laboratory (RSEL)
A hybrid requirements analysis methodology was developed, based on the practices actually used in developing a Space Generic Open Avionics Architecture. During the development of this avionics architecture, a method of analysis able to effectively define the requirements for this space avionics architecture was developed. In this methodology, external interfaces and relationships are defined, a static analysis resulting in a static avionics model was developed, operating concepts for simulating the requirements were put together, and a dynamic analysis of the execution needs for the dynamic model operation was planned. The systems engineering approach was used to perform a top down modified structured analysis of a generic space avionics system and to convert actual program results into generic requirements. CASE tools were used to model the analyzed system and automatically generate specifications describing the model's requirements. Lessons learned in the use of CASE tools, the architecture, and the design of the Space Generic Avionics model were established, and a methodology notebook was prepared for NASA. The weaknesses of standard real-time methodologies for practicing systems engineering, such as Structured Analysis and Object Oriented Analysis, were identified.
Demonstration plan for real time receiving and processing of flight data from the space transportation system
This report presents a detailed demonstration test plan for receiving and processing data from experiments being conducted on the Space Transportation System near real time at the NASA Langley Research Center (LaRC). This task can readily be achieved using the Orbital Acceleration Research Experiment (OARE). The Space Shuttle data flow is described including both the payload and the mission data. A description is presented of the OARE instrument which is used to measure low frequency Space Shuttle accelerations in nano-gs. Procedures are shown for obtaining the required mission data and OARE payload data at LaRC. The demonstration test plan schedule and costs are presented. It is recommended that both the OARE data and the pertinent Space Shuttle mission data be received at LaRC over the NASA Communication System (NASCOM) on a near real time basis.
Unsteady blade pressures on a propfan at takeoff - Euler analysis and flight data
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A simplified method for determining from flight data the rate of change of yawing-moment coefficient with sideslip
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Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data
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An analysis of the errors in curve-fitting problems with an application to the calculation of stability parameters from flight data
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Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data
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Application of several methods for determining transfer functions and frequency response of aircraft from flight data
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