MODELING OF AIRCRAFT PERFORMANCE FROM FLIGHT TEST RESULT USING QUASI STEADY-STATE TEST TECHNIQUES
Material type:
TextPublication details: Kansas Kansas University 1984Description: xviii,416Subject(s): DDC classification: - 629.13453 Ye35m
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | 629.13453 Ye35m (Browse shelf(Opens below)) | Link to resource | Available | A100492 |
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| 629.13453 W211i INTRODUCTION TO FLIGHT TEST ENGINEERING | 629.13453 W211i INTRODUCTION TO FLIGHT TEST ENGINEERING | 629.13453 W211i INTRODUCTION TO FLIGHT TEST ENGINEERING | 629.13453 Ye35m MODELING OF AIRCRAFT PERFORMANCE FROM FLIGHT TEST RESULT USING QUASI STEADY-STATE TEST TECHNIQUES | 629.13457 D475ai4 AIRCRAFT WEIGHT AND BALANCE CONTROL | 629.13457 M56 MEASUREMENT OF THE HANDLING CHARACTERISTICS OF TWO LIGHT AIRPLANES | 629.13457 Sch14 AIRCRAFT WEIGHT AND BALANCE |
Thesis (Ph. D.) -- University Of Kansas, 1984
Photocopy Of The Typescript, Ann Arbor University Microfilm International
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