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NAS 1.60:2535
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Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops |
1 |
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NAS 1.60:2538
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Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facility |
1 |
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NAS 1.60:2544
|
Dynamic response of film thickness in spiral-groove face seals |
1 |
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NAS 1.60:2548
|
Symmetry considerations in the scattering of identical composite bodies |
1 |
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NAS 1.60:2549
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Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap |
1 |
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NAS 1.60:2552
|
Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft |
1 |
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NAS 1.60:2554
|
Programmable, automated transistor test system |
1 |
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NAS 1.60:2555
|
Optical elements formed by compressed gases : analysis and potential applications |
1 |
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NAS 1.60:2557
|
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets |
1 |
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NAS 1.60:2558
|
Technology for Brayton-cycle space powerplants using solar and nuclear energy |
1 |
|
NAS 1.60:2559
|
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability |
1 |
|
NAS 1.60:2562
|
Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery |
1 |
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NAS 1.60:2564
|
Theoretical three-and four-axis gimbal robot wrists |
1 |
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NAS 1.60:2565
|
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel |
1 |
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NAS 1.60:2569
|
Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests |
1 |
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NAS 1.60:2575
|
Graphical techniques to assist in pointing and control studies of orbiting spacecraft |
1 |
|
NAS 1.60:2577
|
Pocketing mechanics of SRM nozzle liner |
1 |
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NAS 1.60:2578
|
Oxidation and emittance of superalloys in heat shield applications |
1 |
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NAS 1.60:2579
|
Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration |
1 |
|
NAS 1.60:2580
|
Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 |
1 |