tailieunhanh - Thiết kế máy bay_Chương VII

Tham khảo sách 'thiết kế máy bay_chương vii', kỹ thuật - công nghệ, cơ khí - chế tạo máy phục vụ nhu cầu học tập, nghiên cứu và làm việc hiệu quả | TECNìCa 5 IM 0 AIRPLANE DESIGN PART VII DETERMINATION OF STABILITY CONTROL AND SSESSSSSS58S3SS SXS SSSBSSSS ESSSBSSBKCKBBKS S SS8SSBaS87SSS8SS PERFORMANCE CHARACTERISTICS FAR AND MILITARY BBSSSBSSSSSKSSKS BSBBSBBaBBiKBCSKSKaBSBBecaSBSBBBSaEXSBB EBK REQUIREMENTS SSSBaBSBBKKBBB - by Dr. Jan Roskam Ackers Distinguished Professor of Aerospace Engineering The University of Kansas Lawrence Kansas NO PART OF THIS BOOK MAY BE REPRODUCED WITHOUT PERMISSION FROM THE AUTHOR Copyright Roskam Aviation and Engineering Corporation Rt4 Box 274 Ottawa Kansas 66067 Tel. 913-2421624 First Printing 1988 TABLE OF CONTENTS SBSSBSKSSSSasaBSSSSSK TABLE OF SYMBOLS vii ACKNOWLEDGEMENT xviii 1. INTRODUCTION 1 2. CONTROLLABILITY MANEUVERABILITY AND TRIM 5 LONGITUDINAL CONTROLLABILITY AND TRIM 7 Applicable Regulations 7 Relationship to Preliminary Design 7 Mathematical Model for Analyzing Longi- tudinal Controllability and Trim 7 Step-by-step Procedure for Analyzing Longitudinal Controllability and Trim 12 DIRECTIONAL AND LATERAL CONTROLLABILITY AND TRIM 19 Applicable Regulations 19 Relationship to Preliminary Design 19 Mathematical Model for Analyzing Directional and Lateral Controllability and Trim 19 Step-by-step Procedure for Analyzing Directional and Lateral Controllability and Trim 22 MINIMUM CONTROL SPEED 26 Applicable Regulations 26 Relationship to Preliminary Design 26 Mathematical Model for Analyzing Minimum Control Speed 26 Step-by-step Procedure for Determining the Minimum Control Speed 27 MANEUVERING FLIGHT 30 Applicable Regulations 30 Relationship to Preliminary Design 30 Mathematical Model for Analyzing Maneuvering Flight 30 Step-bystep Procedure for Determining Maneuvering Flight Ability 33 CONTROL DURING THE TAKEOFF GROUNDRUN 36 Applicable Regulations 36 Relationship to Preliminary Design 36 Mathematical Model for Analyzing Control During the .