| Type of Material: | Thesis |
| Title: | Development of a three-degree-of-freedom elastically forced oscillation rig for the measurement of direct and coupled dynamic stabillity derivatives of aircraft and missile models |
| Researcher: | Srinivasa Rao, B R |
| Guide: | Rao, G N V |
| Department: | Department of Aerospace Engineering |
| Publisher: | Indian Institute of Science |
| Place: | Bangalore |
| Year: | 1989 |
| Language: | English |
| Subject: | Engineering | Aerospace Engineering | Aerodynamics | Stability and Control | Aerospace Engineering |
| Dissertation/Thesis Note: | PhD |
| 000 | 00000ntm a2200000ua 4500 | |
| 001 | 81876 | |
| 003 | IN-AhILN | |
| 005 | 2011-01-13 00:00:00 | |
| 008 | __ | 891231t1989||||ii#||||g|m||||||||||eng|| |
| 035 | __ | |a(IN-AhILN)th_81876 |
| 040 | __ | |aIISC_560012|dIN-AhILN |
| 041 | __ | |aeng |
| 100 | __ | |aSrinivasa Rao, B R|eResearcher |
| 110 | __ | |aDepartment of Aerospace Engineering|bIndian Institute of Science|dBangalore|eIn |
| 245 | __ | |aDevelopment of a three-degree-of-freedom elastically forced oscillation rig for the measurement of direct and coupled dynamic stabillity derivatives of aircraft and missile models |
| 260 | __ | |aBangalore|bIndian Institute of Science|c1989 |
| 502 | __ | |bPhD |
| 650 | __ | |aAerospace Engineering|2UGC |
| 653 | __ | |aEngineering |
| 653 | __ | |aAerospace Engineering |
| 653 | __ | |aAerodynamics |
| 653 | __ | |aStability and Control |
| 700 | __ | |aRao, G N V|eGuide |
| 905 | __ | |anotification |
User Feedback Comes Under This section.