NAS 1.26:2715
|
A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development / |
1 |
NAS 1.26:2716
|
A computational system for aerodynamic design and analysis of supersonic aircraft : part 2, user's manual / |
1 |
NAS 1.26:2717
|
A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description / |
1 |
NAS 1.26:2718
|
Structure-property relationships in low-temperature adhesives / |
1 |
NAS 1.26:2719
|
Plasma core reactor simulations using RF uranium seeded argon discharges / |
1 |
NAS 1.26:2720
|
Development of an optimal automatic control law and filter algorithm for steep glideslope capture and glideslope tracking / |
1 |
NAS 1.26:2721
|
Analysis and testing of two-dimensional vented Coanda ejectors with asymmetric variable area mixing sections / |
1 |
NAS 1.26:2723
|
Applicability of the control configured design approach to advanced earth orbital transportation systems / |
1 |
NAS 1.26:2724
|
Investigation of Kevlar fabric-based materials for use with inflatable structures / |
1 |
NAS 1.26:2725
|
Equilibrium chemical reaction of supersonic hydrogen-air jets : Alma computer program / |
1 |
NAS 1.26:2726
|
A single field of view method for retrieving tropospheric temperature profiles from cloud-contaminated radiance data / |
1 |
NAS 1.26:2727
|
Analysis of structural dynamic data from Skylab / |
1 |
NAS 1.26:2728
|
Analysis of structural dynamic data from Skylab / |
1 |
NAS 1.26:2729
|
Boundary-fitted curvilinear coordinate systems for solution of partial differential equations on fields containing any number of arbitrary two-dimensional bodies / |
1 |
NAS 1.26:2730
|
MIDAS, prototype Multivariate Interactive Digital Analysis System for large area earth resources surveys / |
1 |
NAS 1.26:2731
|
Eigenvalue extraction in NASTRAN by the Tridiagonal Reduction (FEER) Method : real eigenvalue analysis / |
1 |
NAS 1.26:2732
|
Some inconsistencies of the finite element method as applied to inelastic response / |
1 |
NAS 1.26:2733
|
Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence / |
1 |
NAS 1.26:2734
|
A technique for generating arbitrarily shaped curved approach paths / |
1 |
NAS 1.26:2735
|
Higher-order numerical methods derived from three-point polynomial interpolation / |
1 |