APPLICATION OF LINEAR QUADRATIC CONTROL IN REDUCTION OF AERODYNAMIC FORCES ON AIRCRAFT
Material type:
- 629.1323 W435a
Item type | Current library | Collection | Call number | URL | Status | Date due | Barcode | Item holds | |
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | 629.1323 W435a (Browse shelf(Opens below)) | Link to resource | Available | A100899 |
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629.1323 SY68F SYMPOSIUM ON AERODYNAMICS AND AEROACOUSTICS | 629.1323 Sy68s Symposium on high speed aerodynamics | 629.1323 V759f FLIGHT MECHANICS OF HIGH-PERFORMANCE AIRCRAFT | 629.1323 W435a APPLICATION OF LINEAR QUADRATIC CONTROL IN REDUCTION OF AERODYNAMIC FORCES ON AIRCRAFT | 629.1323 W836S Similitude Requirements and Scaling Relationships as Applied to Model Testing [NASA Technical Paper 1435] | 629.1323 W893C CURRENT TOPICS IN NONSTATIONARY ANALYSIS | 629.132300151 D787M MATHEMATICAL METHODS IN AERODYNAMICS |
Facsimile Of : Microfilm Master Copy Of The Original. Ann Arbor : Umi, 1988
Thesis : (Ph.D.) -- Organ State University, 1981
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