Rotor Systems Research Aircraft Airplane Configuration Flight Test Results
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: |
Total Pages |
: 18 |
Release |
: 1984 |
ISBN-10 |
: NASA:31769000562077 |
ISBN-13 |
: |
Rating |
: 4/5 (77 Downloads) |
Synopsis Rotor Systems Research Aircraft Airplane Configuration Flight-test Results by :
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Total Pages |
: 128 |
Release |
: 1986 |
ISBN-10 |
: NASA:31769000566722 |
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: |
Rating |
: 4/5 (22 Downloads) |
Synopsis NASA Rotor Systems Research Aircraft: Fixed-wing Configuration Flight-test Results by :
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Total Pages |
: 22 |
Release |
: 1985 |
ISBN-10 |
: NASA:31769000566490 |
ISBN-13 |
: |
Rating |
: 4/5 (90 Downloads) |
Synopsis Flight Testing the Fixed-wing Configuration of the Rotor Systems Research Aircraft (RSRA) by :
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Total Pages |
: 22 |
Release |
: 1983 |
ISBN-10 |
: NASA:31769000561541 |
ISBN-13 |
: |
Rating |
: 4/5 (41 Downloads) |
Synopsis Flight Testing the Rotor Systems Research Aircraft (RSRA) by :
Author |
: Timothy R. Moes |
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: |
Total Pages |
: 98 |
Release |
: 2002 |
ISBN-10 |
: NASA:31769000451636 |
ISBN-13 |
: |
Rating |
: 4/5 (36 Downloads) |
Synopsis Stability and Control Estimation Flight Test Results for the SR-71 Aircraft With Externally Mounted Experiments by : Timothy R. Moes
A maximum-likelihood output-error parameter estimation technique is used to obtain stability and control derivatives for the NASA Dryden Flight Research Center SR-71A airplane and for configurations that include experiments externally mounted to the top of the fuselage. This research is being done as part of the envelope clearance for the new experiment configurations. Flight data are obtained at speeds ranging from Mach 0.4 to Mach 3.0, with an extensive amount of test points at approximately Mach 1.0. Pilot-input pitch and yaw-roll doublets are used to obtain the data. This report defines the parameter estimation technique used, presents stability and control derivative results, and compares the derivatives for the three configurations tested. The experimental configurations studied generally show acceptable stability, control, trim, and handling qualities throughout the Mach regimes tested.
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Total Pages |
: 1572 |
Release |
: 1992 |
ISBN-10 |
: UIUC:30112078757413 |
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: |
Rating |
: 4/5 (13 Downloads) |
Synopsis Scientific and Technical Aerospace Reports by :
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Total Pages |
: 20 |
Release |
: 1983 |
ISBN-10 |
: NASA:31769000561624 |
ISBN-13 |
: |
Rating |
: 4/5 (24 Downloads) |
Synopsis Rotor Systems Research Aircraft: Fixed-wing Simulations Results by :
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Total Pages |
: 1014 |
Release |
: 1966-11 |
ISBN-10 |
: NYPL:33433066455514 |
ISBN-13 |
: |
Rating |
: 4/5 (14 Downloads) |
Synopsis U.S. Government Research & Development Reports by :
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Total Pages |
: 36 |
Release |
: 1980-05 |
ISBN-10 |
: UIUC:30112101565627 |
ISBN-13 |
: |
Rating |
: 4/5 (27 Downloads) |
Synopsis Army R, D & A. by :
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: |
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: |
Total Pages |
: 1388 |
Release |
: 1971 |
ISBN-10 |
: OSU:32437010583744 |
ISBN-13 |
: |
Rating |
: 4/5 (44 Downloads) |
Synopsis Monthly Catalog of United States Government Publications by :