|
NAS 1.15:3470
|
Pressure distributions induced by elevon deflections on swept wings and adjacent end-plate surfaces at Mach 6 / |
1 |
|
NAS 1.15:3471
|
Air cooling of disk of a solid integrally cast turbine rotor for an automotive gas turbine / |
1 |
|
NAS 1.15:3472
|
Effects of reset stators and a rotating, grooved stator hub on performance of a 1.92-pressure-ratio compressor stage / |
1 |
|
NAS 1.15:3473
|
Mass study for modular approaches to a solar electric propulsion module / |
1 |
|
NAS 1.15:3475
|
Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70ĚŠ swept delta wing / |
1 |
|
NAS 1.15:3476
|
A wind-tunnel investigation of an unpowered helicopter fuselage model with a V-type empennage / |
1 |
|
NAS 1.15:3477
|
Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5 / |
1 |
|
NAS 1.15:3478
|
Analytical procedure for evaluating speckle-effect instrumentation / |
1 |
|
NAS 1.15:3479
|
Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment / |
1 |
|
NAS 1.15:3480
|
Communications technology satellite output-tube design and development / |
1 |
|
NAS 1.15:3481
|
Cold-air performance of a tip turbine designed to drive a lift fan : II, partical admission / |
1 |
|
NAS 1.15:3482
|
Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine / |
1 |
|
NAS 1.15:3483
|
Mechanical characteristics of stability-bleed valves for a supersonic inlet / |
1 |
|
NAS 1.15:3484
|
Application of differential similarity to finding nondimensional groups important in tests of cooled engine components / |
1 |
|
NAS 1.15:3485
|
A heavy ion beam probe system for investigation of a modified penning discharge / |
1 |
|
NAS 1.15:3486
|
OAST space theme workshop / |
1 |
|
NAS 1.15:3488
|
Reevaluation of compressible-flow Preston tube calibrations / |
1 |
|
NAS 1.15:3489
|
Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft / |
1 |
|
NAS 1.15:3490
|
A survey of compiler development aids / |
1 |
|
NAS 1.15:3491
|
Computer simulation incorporating a helicopter model for evaluation of aircraft avionics systems / |
1 |
