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NAS 1.26:2592
|
Radar derived spatial statistics of summer rain / |
1 |
|
NAS 1.26:2593
|
Ditching investigation of a 1/20-scale model of the space shuttle orbiter / |
1 |
|
NAS 1.26:2594
|
Fire safety : a case study of technology transfer / |
1 |
|
NAS 1.26:2595
|
Control of shock wave - boundary layer interactions by bleed in supersonic mixed compression inlets / |
1 |
|
NAS 1.26:2597
|
Design, fabrication and acoustic tests of a 36 inch (0.914 meter) statorless turbotip fan / |
1 |
|
NAS 1.26:2598
|
Atmospheric scavenging of hydrochloric acid / |
1 |
|
NAS 1.26:2599
|
Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings / |
1 |
|
NAS 1.26:2600
|
Emotionality in response to aircraft noise : a report of developmental work / |
1 |
|
NAS 1.26:2601/
|
Carbide coated fibers in graphite-aluminum composites : progress report / |
1 |
|
NAS 1.26:2602
|
Prediction of span loading of straight-wing/propeller combinations up to stall / |
1 |
|
NAS 1.26:2603
|
A preliminary investigation of the potential applicability of the IPAD system to non-aerospace industry / |
1 |
|
NAS 1.26:2604
|
High Reynolds number tests of a C141A aircraft semispan model to investigate shock-induced separation / |
1 |
|
NAS 1.26:2605
|
A passive gust alleviation system for a light aircraft / |
1 |
|
NAS 1.26:2607
|
Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft / |
1 |
|
NAS 1.26:2608
|
Grown organic matter as a fuel raw material resource / |
1 |
|
NAS 1.26:2609
|
Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft / |
1 |
|
NAS 1.26:2610
|
Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration / |
1 |
|
NAS 1.26:2611
|
Prediction of rotating-blade vortex noise from noise of nonrotating blades / |
1 |
|
NAS 1.26:2612
|
Aircraft motion and passenger comfort data from scheduled commercial airline flights / |
1 |
|
NAS 1.26:2613
|
Comosite engines for application to a single-stage-to-orbit vehicle / |
1 |
