| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.15:4697 | Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5 | 1 |
| NAS 1.15:4698 |
Performance trend of different algorithms for structural design optimization / Performance trend of different algorithms for structural design optimization |
2 |
| NAS 1.15:4700 | Scheduling logic for miles-in-trail traffic management | 1 |
| NAS 1.15:4703 | The NASA landing gear test airplane | 1 |
| NAS 1.15:4704 | Flight test validation of a frequency-based system identification method on an F-15 aircraft | 1 |
| NAS 1.15:4705 | Flight assessment of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft | 1 |
| NAS 1.15:4706 | Spacelab Life Sciences-1 final report / | 1 |
| NAS 1.15:4714 |
Artificial boundary conditions for computation of oscillating external flows Artificial boundary conditions for computation of oscillating external flows / |
2 |
| NAS 1.15:4715 | The NASA/MSFC global reference atmospheric model--1995 version (GRAM-95) / | 1 |
| NAS 1.15:4719 |
Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf |
2 |
| NAS 1.15:4720 | A historical overview of flight flutter testing / | 1 |
| NAS 1.15:4721 | Least squares best fit method for the three parameter Weibull distribution : analysis of tensile and bend specimens with volume or surface flaw failure / | 1 |
| NAS 1.15:4722 | Design and development of an F/A-18 inlet distortion rake : a cost and time saving solution / | 1 |
| NAS 1.15:4724 |
Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code / Progressive Damage Analysis of Laminated Composite (PDALC)--a computational model implemented in the NASA COMET finite element code |
2 |
| NAS 1.15:4726 |
Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle Subsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle / |
2 |
| NAS 1.15:4727 |
Pilot evaluations of runway status light system / Pilot evaluations of runway status light system |
2 |
| NAS 1.15:4728 | A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients | 1 |
| NAS 1.15:4729 |
Dynamic analysis with stress mode animation by the integrated force method Dynamic analysis with stress mode animation by the integrated force method / |
2 |
| NAS 1.15:4736 | Acoustic survey of a 3/8-scale automotive wind tunnel | 1 |
| NAS 1.15:4737 |
Second United States microgravity payload one year report / Second United States microgravity payload : one year report / |
2 |
