| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.15:4772 |
An overview of the NASA F-18 High Alpha Research Vehicle An overview of the NASA F-18 high alpha research vehicle / |
2 |
| NAS 1.15:4773 |
High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle / High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle |
2 |
| NAS 1.15:4774 |
Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV / |
2 |
| NAS 1.15:4775 |
Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment / |
2 |
| NAS 1.15:4776 |
Wrist camera orientation for effective telerobotic Orbital Replaceable Unit (ORU) changeout Wrist camera orientation for effective telerobotic Orbital Replaceable Unit (ORU) changeout / |
2 |
| NAS 1.15:4777 | Design and laboratory validation of a capacitive sensor for measuring the recession of a thin-layered ablator | 1 |
| NAS 1.15:4779 |
Quasi-static viscoelasticity loading measurements of an aircraft tire Quasi-static viscoelasticity loading measurements of an aircraft tire / |
2 |
| NAS 1.15:4782 |
F-15B/flight test fixture II a test bed for flight research / F-15B/flight test fixture II : a test bed for flight research / |
2 |
| NAS 1.15:4783 |
The F/A-18 high-angle-of-attack ground-to-flight correlation lessons learned / The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned / |
2 |
| NAS 1.15:4784 |
An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses / |
2 |
| NAS 1.15:4786 |
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack / |
2 |
| NAS 1.15:4787 |
Thermal conductivity database of various structural carbon-carbon composite materials Thermal conductivity database of various structural carbon-carbon composite materials / |
2 |
| NAS 1.15:4789 |
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing / Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing |
2 |
| NAS 1.15:4790 |
PLATSIM a simulation and analysis package for large-order flexible systems (version 2.0) / PLATSIM : a simulation and analysis package for large-order flexible systems (version 2.0) / |
2 |
| NAS 1.15:4791 |
Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data / |
2 |
| NAS 1.15:4792 |
Overview of recent flight flutter testing research at NASA Dryden Overview of recent flight flutter testing research at NASA Dryden / |
2 |
| NAS 1.15:4793 |
Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data / |
2 |
| NAS 1.15:4795 |
STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program / STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program |
2 |
| NAS 1.15:4796 |
Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements |
2 |
| NAS 1.15:4799 |
Dynamic ground effect for a cranked arrow wing airplane Dynamic ground effect for a cranked arrow wing airplane / |
2 |
