5 results on '"Buchanan, T."'
Search Results
2. Description of a new high-alpha, high-load, pitch-yaw dynamic stability test mechanism at AEDC
3. Aerodynamic lag of a close-coupled canard aircraft model at Mach 0.3to 1.6
4. LOWER EXTREMITY STIFFNESS IN RUNNERS WITH DIFFERENT FOOT TYPES.
5. LIMITATIONS OF INVERSE DYNAMICS IN IDENTIFYING QUADRICEPS AVOIDANCE.
Catalog
Books, media, physical & digital resources
Discovery Service for Jio Institute Digital Library
For full access to our library's resources, please sign in.