NAS 1.26:3663
|
Design concepts for large reflector antenna structures / |
1 |
NAS 1.26:3664
|
Development of aerodynamic prediction methods for irregular planform wings / |
1 |
NAS 1.26:3665
|
Comparison of foward flight effects theory of A. Michalke and U. Michel with measured data / |
1 |
NAS 1.26:3666
|
The effectiveness of an oculometer training tape on pilot and copilot trainees in a commercial flight training program / |
1 |
NAS 1.26:3667
|
The effectiveness of incorporating a real-time oculometer system in a commercial flight training program / |
1 |
NAS 1.26:3668
|
ADAM, an axisymmetric duct aeroacoustic modeling system / |
1 |
NAS 1.26:3669
|
Numerical studies of laminar and turbulent drag reduction : part II / |
1 |
NAS 1.26:3670
|
A Study of the stress wave factor technique for the characterization of composite materials / |
1 |
NAS 1.26:3671
|
End wall flow characteristics and overall performance of an axial flow compressor stage / |
1 |
NAS 1.26:3672
|
Synthesized airfoil data method for predicttion of dynamic stall and unsteady airloads |
1 |
NAS 1.26:3673
|
Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics / |
1 |
NAS 1.26:3674
|
Test results of modified electrical charged particle generator for application to fog dispersal / |
1 |
NAS 1.26:3675
|
An aerodynamic analysis computer program and design notes for low speed wing flap systems |
1 |
NAS 1.26:3676
|
The COREL and W12SC3 computer programs for supersonic wing design and analysis / |
1 |
NAS 1.26:3678
|
Flight in low-level wind shear / |
1 |
NAS 1.26:3679
|
Effects of specimen resonances on acoustic-ultrasonic testing / |
1 |
NAS 1.26:3680
|
Plasma-sprayed self-lubricating coatings / |
1 |
NAS 1.26:3681/
|
Terminal area automatic navigation, guidance control research using the microwave landing system (MLS) / |
1 |
NAS 1.26:3682
|
Shear-lag analysis of a hybrid, unidirectional composite with fiber damage / |
1 |
NAS 1.26:3683
|
Analysis and test for space shuttle propellant dynamics / |
1 |