Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:110280 |
Composite interlaminar shear fracture toughness, G[sub IIc] : shear measurement or sheer myth? / Composite interlaminar shear fracture toughness, G[sub IIc] shear measurement or sheer myth? / |
2 |
NAS 1.15:110281 | Performance of optimized actuator and sensor arrays in an active noise control system | 1 |
NAS 1.15:110282 |
A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet / A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet |
2 |
NAS 1.15:110283 |
Finite difference radiative transfer model calculations compared to measurements at the top and bottom of the atmosphere / Finite difference radiative transfer model calculations compared to measurements at the top and bottom of the atmosphere |
2 |
NAS 1.15:110284 | Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method | 1 |
NAS 1.15:110285 |
The Kirchhoff formulas for moving surfaces in aeroacoustics the subsonic and supersonic cases / The Kirchhoff formulas for moving surfaces in aeroacoustics : the subsonic and supersonic cases / |
2 |
NAS 1.15:110286 |
Properties of two carbon composite materials using LTM25 epoxy resin / Properties of two carbon composite materials using LTM25 epoxy resin |
2 |
NAS 1.15:110287 |
Robust stabilization of a class of passive nonlinear systems Robust stabilization of a class of passive nonlinear systems / |
2 |
NAS 1.15:110289 |
Comparisons of methods for predicting community annoyance due to sonic booms / Comparisons of methods for predicting community annoyance due to sonic booms |
2 |
NAS 1.15:110290 |
Integration of multiple non-normal checklist procedures into a single checklist procedure for transport aircraft : a preliminary investigation / Integration of multiple non-normal checklist procedures into a single checklist procedure for transport aircraft a preliminary investigation / |
2 |
NAS 1.15:110291 |
A benchmark problem for development of autonomous structural modal identification / A benchmark problem for development of autonomous structural modal identification |
2 |
NAS 1.15:110292 |
Asymptotic Waveform Evaluation (AWE) technique for frequency domain electromagnetic analysis / Asymptotic Waveform Evaluation (AWE) technique for frequency domain electromagnetic analysis |
2 |
NAS 1.15:110293 |
Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / |
2 |
NAS 1.15:110294 |
User's guide for flight simulation data visualization workstation / User's guide for flight simulation data visualization workstation |
2 |
NAS 1.15:110295 |
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure |
2 |
NAS 1.15:110296 |
Development of metallic thermal protection systems for the reusable launch vehicle / Development of metallic thermal protection systems for the reusable launch vehicle |
2 |
NAS 1.15:110298 | Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data | 1 |
NAS 1.15:110300 |
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / |
2 |
NAS 1.15:110302 |
Compression response of a sandwich fuselage keel panel with and without damage / Compression response of a sandwich fuselage keel panel with and without damage |
2 |
NAS 1.15:110303 |
Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets / |
2 |