NAS 1.14:D-4982
|
Quantum theory of a particle-oscillator collision applied to gas-surface interactions at cryogenic temperatures / |
1 |
NAS 1.14:D-4983
|
Full-scale wind-tunnel investigation of static longitudinal and lateral characteristics of a light twin-engine airplane / |
1 |
NAS 1.14:D-4984
|
Dynamic response of hydrazine-nitrogen tetroxide combustion to transverse gas flow / |
1 |
NAS 1.14:D-4985
|
Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel / |
1 |
NAS 1.14:D-4986
|
An optical system for recording schlieren images with a continuous-writing ultra-high-speed framing camera / |
1 |
NAS 1.14:D-4987
|
Flight performance of FW-4D solid-propellant rocket motor on Delta 50 (AIMP-E) / |
1 |
NAS 1.14:D-4990
|
Effects of structural damping on flutter or stressed panels / |
1 |
NAS 1.14:D-4991
|
Nonequilibrium calculations of methane-fluorine-oxygen and butene-1-fluorine-oxygen rocket performance / |
1 |
NAS 1.14:D-4992
|
Theoretical nonequilibrium performance of oxygen difluoride-diborane rocket propellant / |
1 |
NAS 1.14:D-4993
|
Components of a hydrogen plasma including minor species / |
1 |
NAS 1.14:D-4994
|
The effect of orientation and the presence of surface active materials on the friction, deformation and wear of aluminum / |
1 |
NAS 1.14:D-4995
|
Analysis and design of inductors for protecting power transistors against current surges in inverter bridge circuits / |
1 |
NAS 1.14:D-4996
|
Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions / |
1 |
NAS 1.14:D-4997
|
Error analysis of input-noise-temperature measurements of low-noise amplifiers / |
1 |
NAS 1.14:D-4998
|
Crack toughness characteristics of several alloys for use in heavy sections of high speed aircraft / |
1 |
NAS 1.14:D-4999
|
A survey of salt deposits in compressors of flight gas turbine engines / |
1 |
NAS 1.14:D-5000
|
Hot-salt stress-corrosion of titanium alloys : generation of hydrogen and its embrittling effect / |
1 |
NAS 1.14:D-5001
|
Analytical study of flow reduction due to oxidation of wire-form porous sheet for transpiration cooled turbine blades / |
1 |
NAS 1.14:D-5002
|
Rolling-element bearing life from 400 ̊to 600 ̊F / |
1 |
NAS 1.14:D-5003
|
Preliminary study of effects of reynolds number and boundary-layer transition location on shock-induced separation / |
1 |