|
NAS 1.14:D-7619
|
Evaluation of tantalum-alloy-clad uranium mononitride fuel specimens from 7500-hour, 1040̊ C pumped-lithium-loop test / |
1 |
|
NAS 1.14:D-7621
|
REDUCE II - a computer program for the symbolic reduction of large block diagrams / |
1 |
|
NAS 1.14:D-7622
|
Curve fits of predicted inviscid stagnation-point radiative heating rates, cooling factors, and shock standoff distances for hyperbolic earth entry / |
1 |
|
NAS 1.14:D-7623
|
Further analysis of broadband noise measurements for a rotating blade operating with and without its shed wake blown downstream / |
1 |
|
NAS 1.14:D-7624
|
Helicopter rotor rotational noise predictions based on measured high-frequency blade loads / |
1 |
|
NAS 1.14:D-7625
|
Turbine for a low-cost turbojet engine / |
1 |
|
NAS 1.14:D-7626
|
Turbine for a low-cost turbojet engine / |
1 |
|
NAS 1.14:D-7627
|
A systematic study of focal ratios and effects of optical misalignment for LST / |
1 |
|
NAS 1.14:D-7628
|
Oxidative vaporization kinetics of chromium (III) oxide in oxygen from 1270 to 1570 K / |
1 |
|
NAS 1.14:D-7629
|
Enhancement of oxidative vaporization of chromium (III) oxide and chromium by oxygen atoms. |
1 |
|
NAS 1.14:D-7630
|
Subsonic annular wing theory with application to flow about nacelles / |
1 |
|
NAS 1.14:D-7631
|
Aerodynamic characteristics of three slender sharp-edge 74̊ swept wings at subsonic, transonic, and supersonic Mach numbers / |
1 |
|
NAS 1.14:D-7632
|
Holographic and ultrasonic detection of bond flaws in aluminum panels reinforced with boron-epoxy / |
1 |
|
NAS 1.14:D-7633
|
Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65̊ swept delta wing / |
1 |
|
NAS 1.14:D-7634
|
Diffusion with chemical reaction : an attempt to explain number density anomalies in experiments involving alkali vapor / |
1 |
|
NAS 1.14:D-7635
|
Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) / |
1 |
|
NAS 1.14:D-7636
|
Effect of geometrical and flow parameters on high-effectiveness region of film cooling / |
1 |
|
NAS 1.14:D-7637
|
Application of boundary integral method to elastoplastic analysis of V-notched beams / |
1 |
|
NAS 1.14:D-7638
|
Pressurant requirements for discharge of liquid methane from a 1.52-meter- (5-ft-) diameter spherical tank under both static and slosh conditions / |
1 |
|
NAS 1.14:D-7639
|
Research turbine for high-temperature core engine application / |
1 |
