NAS 1.15:86252
|
Scientific and technical training in the Soviet Union |
1 |
NAS 1.15:86253
|
Telescoping space station modules |
1 |
NAS 1.15:86254
|
Interactive systems design and synthesis of future spacecraft concepts |
1 |
NAS 1.15:86255
|
Management of CAD/CAM information key to improved manufacturing productivity / |
1 |
NAS 1.15:86256
|
Rapid adhesive bonding concepts |
1 |
NAS 1.15:86257
|
Design of a candidate flutter suppression control law for DAST ARW-2 |
1 |
NAS 1.15:86258
|
Some aerodynamic discoveries and related NACA/NASA research programs following World War II |
1 |
NAS 1.15:86259
|
Ground vibration test of F-16 airplane with initial decoupler pylon / |
1 |
NAS 1.15:86260
|
Structural performance of orthogonal tetrahedral truss space-station configurations |
1 |
NAS 1.15:86261
|
The Semi-Markov Unreliability Range Evaluator (SURE) program |
1 |
NAS 1.15:86263
|
A buckling analysis for rectangular orthotropic plates with centrally located cutouts |
1 |
NAS 1.15:86264
|
A route generator concept for aircraft onboard fault monitoring |
1 |
NAS 1.15:86265
|
Galactic heavy-ion shielding using electrostatic fields / |
1 |
NAS 1.15:86266
|
Methods for analysis of cracks in three-dimensional solids |
1 |
NAS 1.15:86269
|
Active controls a look at analytical methods and associated tools / |
1 |
NAS 1.15:86270
|
Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters / |
1 |
NAS 1.15:86271
|
Large deflections of circular isotropic membranes subjected to arbitrary axisymmetric loading |
1 |
NAS 1.15:86272
|
First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner |
1 |
NAS 1.15:86273
|
High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II |
1 |
NAS 1.15:86274
|
Description of the insulation system for the Langley 0.3-meter transonic cryogenic tunnel / |
1 |