Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:85916 | Predicted performance benefits of an adaptive digital engine control system on an F-15 airplane | 1 |
NAS 1.15:85917 | Flutter clearance of the Schweizer 1-36 deep-stall sailplane | 1 |
NAS 1.15:85918 | Comparison of measured and calculated temperatures for a Mach 8 hypersonic wing test structure | 1 |
NAS 1.15:85919 | Development experience with a simple expert system demonstrator for pilot emergency procedures | 1 |
NAS 1.15:85920 | Ground-effect analysis of a jet transport airplane | 1 |
NAS 1.15:85923 | Closing the design loop on HiMAT (highly maneuverable aircraft technology) | 1 |
NAS 1.15:85924 | The western aeronautical test range of NASA Ames Research Center | 1 |
NAS 1.15:85925 | Remote control of an impact demonstration vehicle | 1 |
NAS 1.15:85927 | Formulation and analysis of combat games | 1 |
NAS 1.15:85929 | Biomedical Research Division significant accomplishments for FY 1983 | 1 |
NAS 1.15:85932 | Numerical simulation of the tip vortex off a low-aspect-ratio wing at transonic speed | 1 |
NAS 1.15:85933 | NASA-FAA helicopter microwave landing system curved path flight test | 1 |
NAS 1.15:85934 | Development and application of an analysis of axisymmetric body effects on helicopter rotor aerodynamics using modified slender body theory | 1 |
NAS 1.15:85935 | Hygrothermal influence on delamination behavior of graphite/epoxy laminates | 1 |
NAS 1.15:85936 | V/STOL wind-tunnel testing | 2 |
NAS 1.15:85937 | Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft | 2 |
NAS 1.15:85938 |
V/STOL concepts in the the United States past, present, and future / V/STOL concepts in the United States: Past, present, and future |
2 |
NAS 1.15:85939 | V/STOL maneuverability and control | 1 |
NAS 1.15:85940 | Nonlinear problems in flight dynamics | 1 |
NAS 1.15:85941 | Advanced leading edge thermal-structure concept. Direct bond reusable surface insulation to a composite structure | 1 |