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Flight vehicle performance and aerodynamic control /

Annotation "Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters d...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Smetana, Frederick O., 1928-
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston, Va. : American Institute of Aeronautics and Astronautics, ©2001.
Colección:AIAA education series.
Temas:
Acceso en línea:Texto completo

MARC

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100 1 |a Smetana, Frederick O.,  |d 1928-  |1 https://id.oclc.org/worldcat/entity/E39PCjDpGRM68FQXM8Rvd6bkym 
245 1 0 |a Flight vehicle performance and aerodynamic control /  |c Frederick O. Smetana. 
260 |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics,  |c ©2001. 
300 |a 1 online resource (xx, 359 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
347 |a data file  |2 rda 
490 1 |a AIAA education series 
504 |a Includes bibliographical references (pages 355-356) and index. 
506 |3 Use copy  |f Restrictions unspecified  |2 star  |5 MiAaHDL 
533 |a Electronic reproduction.  |b [Place of publication not identified] :  |c HathiTrust Digital Library,  |d 2010.  |5 MiAaHDL 
538 |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.  |u http://purl.oclc.org/DLF/benchrepro0212  |5 MiAaHDL 
583 1 |a digitized  |c 2010  |h HathiTrust Digital Library  |l committed to preserve  |2 pda  |5 MiAaHDL 
520 8 |a Annotation "Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces. This book includes time-tested computer programs that perform the analyses in a manner that reduces student error and improves result accuracy. Because the source code is given, users with a FORTRAN compiler can modify the program to suit particular needs. The major advantage of the software is that more realistic problems may be treated and the effects of parametric programs are more accurate than calculators. The programs are available as executables for Windows machines as well as in ASCII source code versions that can be readily compiled and then executed on Unix, Linux, and Macintosh machines and on mainframes. 
505 0 |a Cover -- Title -- Copyright -- Table of Contents -- Preface -- Why Another Performance Book? -- The Included Software -- Chapter 1. Basic Nomenclature -- Chapter 2. The Atmosphere -- Chapter 3. Characteristics of Power Plants -- Chapter 4. Flight Vehicle Lift-Drag Characteristics -- Chapter 5. Equations of Motion -- Chapter 6. Determination of Aerodynamic Characteristics -- Chapter 7. Flight Vehicle Performance -- Chapter 8. Aerodynamic Control Forces and Static Stability -- Chapter 9. Flight Vehicle Aerodynamic Control 
505 8 |a Appendix A. Pressure, Density, and Temperature Variations with AltitudeAppendix B. Octane Ratings -- Appendix C. Description and Use of Program TRAJECT -- Glossary -- References -- Subject Index 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Airplanes  |x Performance. 
650 0 |a Airplanes  |x Control surfaces. 
650 0 |a Aerodynamics. 
650 6 |a Avions  |x Performances. 
650 6 |a Avions  |x Gouvernes. 
650 6 |a Aérodynamique. 
650 7 |a aerodynamics.  |2 aat 
650 7 |a Aerodynamics  |2 fast 
650 7 |a Airplanes  |x Control surfaces  |2 fast 
650 7 |a Airplanes  |x Performance  |2 fast 
650 7 |a Flugzeugaerodynamik  |2 gnd 
650 7 |a Regelung  |2 gnd 
655 7 |a dissertations.  |2 aat 
655 7 |a Academic theses  |2 fast 
655 7 |a Academic theses.  |2 lcgft 
655 7 |a Thèses et écrits académiques.  |2 rvmgf 
758 |i has work:  |a Flight vehicle performance and aerodynamic control (Text)  |1 https://id.oclc.org/worldcat/entity/E39PCFxgmX6vHdwwRg8JffxrG3  |4 https://id.oclc.org/worldcat/ontology/hasWork 
776 0 8 |i Print version:  |a Smetana, Frederick O., 1928-  |t Flight vehicle performance and aerodynamic control.  |d Reston, VA : American Institute of Aeronautics and Astronautics, ©2001  |w (DLC) 2001022681  |w (OCoLC)46640726 
830 0 |a AIAA education series. 
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