NAS 1.26:2559
|
Numerical nonlinear inelastic analysis of stiffened shells of revolution / |
1 |
NAS 1.26:2560
|
Experimental studies of flow separation and stalling on a two-dimensional airfoil at low speeds / |
1 |
NAS 1.26:2561
|
Application of active controls technology to the NASA JetStar airplane / |
1 |
NAS 1.26:2562
|
Stresses in a webbed ball / |
1 |
NAS 1.26:2563
|
Experimental evaluation of a Mach 3.5 axisymmetric inlet / |
1 |
NAS 1.26:2565
|
Development of a superconductor magnetic suspension and balance prototype facility for studying the feasibility of applying this technique to large scale aerodynamic testing / |
1 |
NAS 1.26:2566/
|
Carbide coated fibers in graphite-aluminum composites : progress report / |
1 |
NAS 1.26:2567
|
An investigation of turbulent transport in the extreme lower atmosphere / |
1 |
NAS 1.26:2568
|
PLANS : a finite element program for nonlinear analysis of structures. |
1 |
NAS 1.26:2569
|
Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel / |
1 |
NAS 1.26:2570
|
Feasibility of miniaturized instrumentation of the inflatable sphere for temperature, pressure and acceleration measurement / |
1 |
NAS 1.26:2571
|
Theory of an airfoil equipped with a jet flap under low-speed flight conditions / |
1 |
NAS 1.26:2572
|
Kinetic description of ionospheric dynamics in the three-fluid approximation / |
1 |
NAS 1.26:2573
|
Analysis of helicopter rotor blade torsional oscillations due to stall / |
1 |
NAS 1.26:2574
|
Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory / |
1 |
NAS 1.26:2575
|
A procedure for standardization of color infrared film response / |
1 |
NAS 1.26:2576
|
Flight effects on noise generated by the JT8D engine in a quiet nacelle and a conventional nacelle as measured in the NASA-AMES 40- by 80-foot wind tunnel : summary report / |
1 |
NAS 1.26:2577
|
Transonic airfoil flowfield analysis using Cartesian coordinates / |
1 |
NAS 1.26:2578
|
Transonic airfoil design using cartesian coordinates / |
1 |
NAS 1.26:2579
|
Ablative heat shield design for space shuttle / |
1 |