NAS 1.15:4101
|
Atmospheric Laboratory for Applications and Science, mission 1 |
1 |
NAS 1.15:4102
|
Procedures for characterizing an alloy and predicting cyclic life with the total strain version of strainrange partitioning |
1 |
NAS 1.15:4103
|
Automating the multiprocessing environment |
1 |
NAS 1.15:4105
|
Rotary balances a selected, annotated bibliography / |
1 |
NAS 1.15:4106
|
Interfacing laboratory instruments to multiuser, virtual memory computers |
1 |
NAS 1.15:4108
|
Lateral stability analysis for X-29A drop model using system identification methodology |
1 |
NAS 1.15:4109
|
Updated users' guide for TAWFIVE with multigrid |
1 |
NAS 1.15:4110
|
Geometrical and structural properties of an aeroelastic research wing (ARW-2) |
1 |
NAS 1.15:4111
|
Transonic Navier-Stokes solutions of three-dimensional afterbody flows |
1 |
NAS 1.15:4112
|
Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters |
1 |
NAS 1.15:4113
|
Computing induced velocity perturbations due to a helicopter fuselage in a free stream |
1 |
NAS 1.15:4114
|
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel |
1 |
NAS 1.15:4115
|
Vibration testing of impact-damaged composite laminates |
1 |
NAS 1.15:4116
|
Flutter of a low-aspect-ratio rectangular wing |
1 |
NAS 1.15:4117
|
Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration |
1 |
NAS 1.15:4118
|
A Hierarchy of transport approximations for high energy heavy (HZE) ions |
1 |
NAS 1.15:4119
|
Application of a PC based, real-time, data-acquisition system in rotorcraft wind-tunnel testing |
1 |
NAS 1.15:4123
|
Evaluation of fault-tolerant parallel-processor architectures over long space missions |
1 |
NAS 1.15:4124
|
Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow |
2 |
NAS 1.15:4125
|
A three-node C ĚŠelement for analysis of laminated composite sandwich shells |
1 |