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NASA-TM-78678

Airplane stability calculations with a card programmable pocket calculato

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1978

Abstract: Programs are presented for calculating airplane stability characteristics with a card programmable pocket calculator. These calculations include eigenvalues of the characteristic equations of lateral and longitudinal motion as well as stability parameters such as the time to damp to one-half amplitude or the damping ratio. The effects of wind shear are included. Background information and the equations programmed are given. The programs are written for the International System of Units, the dimensional form of the stability derivatives, and stability axes. In addition to programs for stability calculations, an unusual and short program is included for the Euler transformation of coordinates used in airplane motions. The programs have been written for a Hewlett Packard HP-67 calculator. However, the use of this calculator does not constitute an endorsement of the product by the National Aeronautics and Space Administration.
URI: https://yse.yabesh.ir/std/handle/yse/136256
Subject: AIRCRAFT STABILITY
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    NASA-TM-78678

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:12:43Z
date available2017-09-04T17:12:43Z
date copyright01/01/1978
date issued1978
identifier otherYWHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/136256
description abstractPrograms are presented for calculating airplane stability characteristics with a card programmable pocket calculator. These calculations include eigenvalues of the characteristic equations of lateral and longitudinal motion as well as stability parameters such as the time to damp to one-half amplitude or the damping ratio. The effects of wind shear are included. Background information and the equations programmed are given. The programs are written for the International System of Units, the dimensional form of the stability derivatives, and stability axes. In addition to programs for stability calculations, an unusual and short program is included for the Euler transformation of coordinates used in airplane motions. The programs have been written for a Hewlett Packard HP-67 calculator. However, the use of this calculator does not constitute an endorsement of the product by the National Aeronautics and Space Administration.
languageEnglish
titleNASA-TM-78678num
titleAirplane stability calculations with a card programmable pocket calculatoen
typestandard
page66
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1978
contenttypefulltext
subject keywordsAIRCRAFT STABILITY
subject keywordsCALCULATORS
subject keywordsDAMPING
subject keywordsDYNAMIC CHARACTERISTICS
subject keywordsEIGENVALUES
subject keywordsHEWLETT-PACKARD COMPUTERS
subject keywordsMATHEMATICAL PROGRAMMING
subject keywordsMOTION STABILITY
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian