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NAS 1.60:3165
|
Annoyance caused by aircraft en route noise / |
2 |
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NAS 1.60:3166
|
A methodology for computing uncertainty bounds of multivariable systems based on sector stability theory concepts |
1 |
|
NAS 1.60:3167
|
A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating |
1 |
|
NAS 1.60:3168
|
Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model |
1 |
|
NAS 1.60:3169
|
Diffracted and head waves associated with waves on nonseparable surfaces / |
2 |
|
NAS 1.60:3170
|
Modeling of the heat transfer in bypass transitional boundary-layer flows |
1 |
|
NAS 1.60:3171
|
Experimental behavior of graphite-epoxy y-stiffened specimens loaded in compression |
1 |
|
NAS 1.60:3172
|
Comparison of jet plume shape predictions and plume influence on sonic boom signature |
1 |
|
NAS 1.60:3173
|
Optimization of composite sandwich cover panels subjected to compressive loadings |
1 |
|
NAS 1.60:3177
|
Optical measurements on solid specimens of solid rocket motor exhaust and solid rocket motor slag |
1 |
|
NAS 1.60:3180
|
Optical communications and a comparison of optical technologies for a high data rate return link from Mars |
1 |
|
NAS 1.60:3181
|
Limit cycle vibrations in turbomachinery |
1 |
|
NAS 1.60:3183
|
Venturi air-jet vacuum ejectors for high-volume atmospheric sampling on aircraft platforms |
1 |
|
NAS 1.60:3184
|
Wind tunnel aerodynamic characteristics of a transport-type airfoil in a simulated heavy rain environment |
1 |
|
NAS 1.60:3185
|
Multiple lesion track structure model |
1 |
|
NAS 1.60:3186
|
Direct simulation of high-speed mixing layers |
1 |
|
NAS 1.60:3187
|
Fault tolerance of artificial neural networks with applications in critical systems |
1 |
|
NAS 1.60:3188
|
Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities |
1 |
|
NAS 1.60:3189
|
Unsteady pressure loads in a generic high-speed engine model |
1 |
|
NAS 1.60:3191
|
Upper stages using liquid propulsion and metallized propellants |
1 |
