Call Number (LC) | Title | Results |
---|---|---|
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 |
NAS 1.15:4738 |
Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight / Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight |
2 |
NAS 1.15:4741 |
Computer program to obtain ordinates for NACA airfoils / Computer program to obtain ordinates for NACA airfoils |
2 |
NAS 1.15:4742 | Characterization of multilayer piezoelectric actuators for use in active isolation mounts / | 2 |
NAS 1.15:4744 |
A comparison of two control display unit concepts on flight management system training / A comparison of two control display unit concepts on flight management system training |
2 |
NAS 1.15:4745 |
Development and flight test of an augmented thrust-only flight control system on an MD- 11 transport airplane / Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane |
2 |
NAS 1.15:4746 |
Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis / Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis |
2 |
NAS 1.15:4747 |
Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis / Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis |
2 |
NAS 1.15:4749 |
Wind-tunnel development of an SR-71 aerospike rocket flight test configuration / Wind-tunnel development of an SR-71 aerospike rocket flight test configuration |
2 |
NAS 1.15:4750 | Utilizing GPS to determine ionospheric delay over the ocean | 1 |
NAS 1.15:4752 |
Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers / Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers |
2 |