NAS 1.15:110159
|
ATLAS-3 correlative measurement opportunities with UARS and surface observations |
1 |
NAS 1.15:110160
|
A finite element propagation model for extracting normal incidence impedance in nonprogressive acoustic wave fields |
1 |
NAS 1.15:110162
|
Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels |
1 |
NAS 1.15:110163
|
An extension of the Lighthill theory of jet noise to encompass refraction and shielding |
1 |
NAS 1.15:110164
|
Manual for a workstation-based generic flight simulation program (LaRCsim), version 1.4 |
1 |
NAS 1.15:110165
|
Analytical comparison of three stiffened panel concepts |
1 |
NAS 1.15:110166
|
The transition of a real-time single-rotor helicopter simulation program to a supercomputer |
1 |
NAS 1.15:110167
|
Defining the IEEE-854 floating-point standard in PVS |
1 |
NAS 1.15:110168
|
An efficiency study of the simultaneous analysis and design of structures |
1 |
NAS 1.15:110170
|
Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box |
1 |
NAS 1.15:110172
|
A manual for pyrotechnic design, development and qualification |
1 |
NAS 1.15:110173
|
A conceptual thermal design study of an electronically scanned thinned array radiometer |
1 |
NAS 1.15:110174
|
Solution of the three-dimensional Helmholtz equation with nonlocal boundary conditions |
1 |
NAS 1.15:110175
|
Structural design using equilibrium programming formulations |
1 |
NAS 1.15:110176
|
Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness |
1 |
NAS 1.15:110178
|
Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S |
1 |
NAS 1.15:110179
|
Emissivity measurements in thin metallized membrane reflectors used for microwave radiometer sensors |
1 |
NAS 1.15:110180
|
NASA/DoD aerospace knowledge diffusion research project. |
1 |
NAS 1.15:110181
|
NASA/DoD aerospace knowledge diffusion research project. |
1 |
NAS 1.15:110182
|
Orbiter rarefied-flow reentry measurements from the OARE on STS-62 |
1 |