|
NAS 1.15:4586
|
Weight minimization of structural components for launch in space shuttle / |
1 |
|
NAS 1.15:4588
|
Modeling of instrument landing system (ILS) localizer signal on runway 25L at Los Angeles International Airport |
1 |
|
NAS 1.15:4590
|
Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane |
1 |
|
NAS 1.15:4591
|
Evaluating the dynamic response of in-flight thrust calculation techniques during throttle transients |
1 |
|
NAS 1.15:4592
|
ASSIST user manual |
1 |
|
NAS 1.15:4593
|
Completed Beltrami-Michell formulation for analyzing radially symmetrical bodies |
1 |
|
NAS 1.15:4594
|
Lunar Ultraviolet Telescope Experiment phase A final report / |
1 |
|
NAS 1.15:4595
|
Controlling forebody asymmetries in flight experience with boundary layer transition strips / |
1 |
|
NAS 1.15:4596
|
Development of a low-aspect ratio fin for flight research experiments |
1 |
|
NAS 1.15:4597
|
Transonic flight test of a laminar flow leading edge with surface excrescences |
1 |
|
NAS 1.15:4598
|
X-29 flight control system lessons learned / |
1 |
|
NAS 1.15:4599
|
Further development and flight test of an autonomous precision landing system using a parafoil |
1 |
|
NAS 1.15:4601
|
Comparison of computational and experimental results for a supercritical airfoil |
1 |
|
NAS 1.15:4602
|
Mach 10 computational study of a three-dimensional scramjet inlet flow field |
1 |
|
NAS 1.15:4603
|
Hydrogen film cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream |
1 |
|
NAS 1.15:4604
|
Dynamic ground effects flight test of an F-15 aircraft |
1 |
|
NAS 1.15:4605
|
On the use of controls for subsonic transport performance improvement overview and future directions / |
1 |
|
NAS 1.15:4607
|
Automatic procedures for computing complete configuration geometry for individual component descriptions |
1 |
|
NAS 1.15:4608
|
Thermo-oxidative stability of graphite/PMR-15 composites effect of fiber surface modification on composite shear properties / |
1 |
|
NAS 1.15:4610
|
Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels |
1 |
