NAS 1.15:104241
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Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system |
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NAS 1.15:104242
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From an automated flight-test management system to a flight-test engineer's workstation |
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NAS 1.15:104243
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Thermal-structural panel buckling tests |
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NAS 1.15:104245
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Piloted simulation study of a balloon-assisted deployment of an aircraft at high altitude |
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NAS 1.15:104246
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In-flight evaluation of aerodynamic predictions of an air-launched space booster |
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NAS 1.15:104247
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Effects of bleed air extraction on thrust levels of the F404-GE-400 turbofan engine |
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NAS 1.15:104249
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Thermal-structural test facilities at NASA Dryden |
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NAS 1.15:104250
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System overview of the NASA Dryden Integrated Test Facility |
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NAS 1.15:104251
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The development of an airborne information management system for flight test |
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NAS 1.15:104252
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Thrust stand evaluation of engine performance improvement algorithms in an F-15 airplane |
1 |
NAS 1.15:104253
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The F-18 High Alpha Research Vehicle a high-angle-of-attack testbed aircraft / |
1 |
NAS 1.15:104254
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Overview of the NASA Dryden Flight Research Facility aeronautical flight projects |
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NAS 1.15:104255
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Flight testing and simulation of an F-15 airplane using throttles for flight control |
1 |
NAS 1.15:104256
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Rapid development of the X-31 simulation to support flight-testing |
1 |
NAS 1.15:104257
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NAS 1.15:104258
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A rule-based system for real-time analysis of control systems |
1 |
NAS 1.15:104259
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Experience with Ada on the F-18 High Alpha Research Vehicle Flight Test Program |
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NAS 1.15:104260
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The constant current loop a new paradigm for resistance signal conditioning / |
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NAS 1.15:104261
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A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft |
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NAS 1.15:104262
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Stratospheric turbulence measurements and models for aerospace plane design |
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