{"text_format":"2","workbook":"xls","n_sheets":1,"sheets":["report2"],"not_rendered":{"charts":0,"images":0,"macros":0,"external_links":1,"defined_names":1,"comments":0,"pivot_tables":0},"unopened":[],"bounds":{"document_bytes":16777216,"sheet_cells":100000,"run_cost":"one","rows_first":2000,"rows_last":500,"rows_between":2000,"halvings":0,"cell_chars":16384,"cell_head_chars":4096},"cells_cut":0,"cells_raw":0,"read":"whole","date_system":"1900","formulas":"cached_only"}

{"sheet":"report2","index":0,"n_rows":28,"n_cols":5,"rows_kept":28,"cut":false,"hidden":false,"merged":[[0,2,0,3],[0,4,0,5],[1,2,1,3],[1,4,1,5],[2,2,2,3],[2,4,2,5],[3,2,3,3],[4,2,4,3],[7,2,7,3],[8,2,8,3],[9,2,9,3],[10,2,10,3],[11,2,11,3],[16,2,16,3],[17,2,17,3],[21,2,21,3]],"flags":["formulas_cached_only"]}
[null,"1.","Record Nr.",null,"UNINA9911006635203321"]
[null,null,"Autore",null,"Ashley Holt"]
[null,null,"Titolo",null,"Engineering analysis of flight vehicles / / Holt Ashley"]
[null,null,"Pubbl/distr/stampa",null,"Mineola, New York : , : Dover Publications, , 2012"]
[null,null,"ISBN",null,"9780486166537"]
[{"$nulls":4},"1-5231-0954-8"]
[{"$nulls":4},"0-486-16653-8"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (774 p.)"]
[null,null,"Collana",null,"Dover Books on Aeronautical Engineering"]
[null,null,"Disciplina",null,"629.132/3"]
[null,null,"Soggetti",null,"Aerodinàmica"]
[{"$nulls":4},"Aerodynamics"]
[{"$nulls":4},"Mechanical Engineering"]
[{"$nulls":4},"Engineering & Applied Sciences"]
[{"$nulls":4},"Aeronautics Engineering & Astronautics"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Description based upon print version of record."]
[{"$nulls":4},"\"This Dover edition, first published in 1992 and reissued in 2012, is an unabridged, corrected republication of the work first published by the Addison-Wesley Publishing Company, Reading, Mass., 1974, in the “Addison-Wesley Aerospace Series\" -- Bibliographical note"]
[null,null,"Nota di contenuto",null,"Cover; Title Page; Copyright Page; Preface; Contents; Chapter 1 The Morphology of Flight Vehicles; 1.1 Introduction; 1.2 Key factors affecting vehicle configuration; 1.3 Some representative flight vehicles; 1.4 Problems; Chapter 2 Equations of Motion for Rigid Flight Vehicles; 2.1 Definitions;  vector and scalar realizations of Newton's second law; 2.2 The tensor of inertia; 2.3 Choice of vehicle axes; 2.4 Orientation of the vehicle relative to the ground ;  flight-path determination; 2.5 Gravitational terms in the equations of motion; 2.6 The state vector"]
[{"$nulls":4},"2.7 Three significant phenomena that have been neglected2.8 Problems; Chapter 3 Introduction to Vehicle Aerodynamics; 3.1 Aerodynamic contributions to X, Z, and MP;  dimensionless coefficients defined; 3.2 Equations of perturbed longitudinal motion ;  categories of problems in flight dynamics; 3.3 Problems; Chapter 4 Aerodynamic Terms for Equations of Motion;  Airloads on Thin Wings; 4.1 lnviscid fluid motion past streamlined shapes; 4.2 Aerodynamic theory for small disturbances from a uniform flow; 4.3 Thin airfoil in two-dimensional, incompressible flow"]
[{"$nulls":4},"4.4 Compressibility correction at subsonic and supersonic speeds4.5 Thin airfoil in two-dimensional supersonic flow; 4.6 Shock-expansion methods for thicker supersonic airfoils; 4.7 Three-dimensional wings in subsonic flight; 4.8 Three-dimensional wings in supersonic flight; 4.9 Problems; Chapter 5 Propulsive Terms-One-Dimensional Analysis of Jet and Rocket Propulsion; 5.1 Turbojet operation;  steady-flow energy equation;  partition of thrust and drag; 5.2 One-dimensional analysis of ideal ramjet and turbojet; 5.3 Rocket propulsion"]
[{"$nulls":4},"5.4 One-dimensional analysis of turbojet with realistic component efficiencies5.5 Actual turbojet performance; 5.6 Problems; Chapter 6 Small-Perturbation Response and Dynamic Stability of Flight Vehicles; 6.1 Equations of motion;  aerodynamic approximations;  stability derivatives; 6.2 Dimensionless equations of motion; 6.3 Estimation of stability derivatives: longitudinal; 6.4 Estimation of stability derivatives : lateral; 6.5 Problems; Chapter 7 Solution of the Small-Perturbation Equations of Motion; 7.1 A simplified look at a lateral response; 7.2 Lateral-directional normal modes"]
[{"$nulls":4},"comparison with the complete lateral equations of motion roots-locus technique; 7.3 Longitudinal stability and response;  exact and approximate properties of the normal modes; 7.4 Handling qualities; 7.5 Problems; Chapter 8 Static Stability, Trim, Static Performance and Related Subjects; 8.1 Impact of stability requirements on design and longitudinal control; 8.2 Static performance; 8.3 Problems; Chapter 9 Dynamic Performance: Boost from Nonrotating and Rotating Planets;  Numerical Integration of Ordinary Differential Equations; 9.1 Introduction"]
[{"$nulls":4},"9.2 Numerical integration of ordinary differential equations"]
[null,null,null,"Sommario/riassunto","\"\"Written by one of the leading aerospace educators of our time, each sentence is packed with information. An outstanding book.\"\" - Private Pilot\"\"Illuminated throughout by new twists in explaining familiar concepts, helpful examples and intriguing 'by-the-ways.' A fine book.\"\" - Canadian Aeronautics and Space JournalThis classic by a Stanford University educator and a pioneer of aerospace engineering introduces the complex process of designing atmospheric flight vehicles. An exploration of virtually every important subject in the fields of subsonic, transonic, supersonic, and hypersonic aerod"]