(۰) دیدگاه
Model Aircraft Aerodynamics
Model Aircraft Aerodynamics, 3rd Ed
By Martin Simons
Publisher: Motorbooks Intl
Number Of Pages: 336
Publication Date: 1995-04
ISBN-10 / ASIN: 1854861212
ISBN-13 / EAN: 9781854861214
دانلود : http://rapidshare.com/files/147561569/Model_Aircraft_Aerodynamics.rar.html
Low-Speed Aerodynamics: From Wing Theory to Panel Methods
Joseph Katz, Allen Plotkin, “Low-Speed Aerodynamics: From Wing Theory to Panel Methods”
McGraw-Hill Companies | 1991 | ISBN: 0070504466 | 632 pages | PDF | 17,3 MB
Download : http://www.mediafire.com/?uexws3×9ddy
These Softwares are used for Airfoil plotting, Airfoil Design and Analysis, Airfoil Lift, Drag and Moment Calculation, Cl, Cd, Cm, Cl/Cd calculation at the quater-cord point. Free Airfoil Design and Plotting software. 3D wing analysis and design softwares and Softwares for RC Airplane wing and airfoil design.
Roncz is a free Eppler Airfoil Program with compressibility Corrections.
Foilgen is a software program which allows the user to construct NACA 4 digit and 5 digit aifoil sections / geometries.
XFoil is a very useful Free Low Reynolds number airfoil design and analysis code written by Mark Drela. Xfoil is a very famous airfoil analysis software whose data can be used to draw pressure profile plots, lift, drag, moment coefficient airfoil plots and more. Xfoil is also a very useful airfoil design code.
LadsonPc is a software program which allows the user to construct NACA 6 digit and 6A digit airfoil sections / geometries.
Macfoil is an airfoil plotting software for model airplane uses. It can also generate foam-cutting templates, entry and exit ramps, washin and washout angles.
Foils 4.2f is a free airfoil software for the manipulation and the plotting of airfoils.
Compufoil3D (Airfoil Template Plotting Modification System) is a very useful and powerful airfoil template design software. Compufoil3D can be used to built foam wings, build-up wings (balsa wings or plywood wings), leading edge shapes and guides as well as different planforms.
Aifoil Design Workshop is a software by TDM which can be used by aircraft designers and aircraft modelers to make there own aircraft plans. The software can be used for plotting and modifying airfoil shapes. Airfoil files can be exported as .DXF to be used in all popular CAD programs. Multiple airfoils can be blended to make an hybrid airfoil.
Desktop Aeronautics provides airfoil design and analysis software used for RC Airplane wing design. Also offers LinAir software for evaluation of wing planforms.
Martin Hepperle provides different airfoils tools and a program to convert airfoil co-ordinates in different formats. MH also provides different airfoil analyzing codes and software tools.
Profili2 is a very powerful and useful airfoil analysis and design program which can be used for finding out the lift, drag, moment, Cl/Cd plots of different airfoils, airfoil drawing and managing at different Reynolds number. Profili2 is an airfoil analysis software program.
Wing designer plus is a software for conceptual design of aircraft or glider wings or model aircraft wings.
Winfoil is a Aeronautical Design software for the designing and analysis of model aircrafts.
Visual Foil by Hanley Innovations is an airfoil and wing design and analysis software
Online Resources
http://adamone.rchomepage.com/ (Beginners guide to R/C designing, building and flying. Includes basic aerodynamics)
http://www.gylesaero.com/aeronerds/index.shtml (Programs for design of aircraft. Free trial)
http://www.ae.uiuc.edu/m-selig/ (Low-speed airfoil tests)
http://www.airfieldmodels.com/inform…ulas/index.htm
(Formulas for model aircraft design. Aspect Ratio, Wing loading, Dihedral, Wing Area, Mean Aerodynamic Chord)
http://www.av8n.com/how/ (Full-Scale Aerodynamics)
http://www.arvelgentry.com/origins_of_lift.htm (Theory of Lift Generation) Thanks, Steve!
http://www.cncplusplus.com/AeroPlot/Aero%20Plot.htm (Program for plotting airfoils in AutoCad. Free.) Thanks, Zedenek!
http://www.cncplusplus.com/ (Companion to Aeroplot, CNC)
http://www.compufoil.com/index.shtml (Airfoil Plotting Program)
http://www.desktopaero.com/appliedae…e/welcome.html (Full-Scale Aerodynamics)
http://www.djaerotech.com/dj_askjd/d…tail_coef.html (Tail Volume Coefficient)
http://www.eskimo.com/~billb/wing/airfoil.html (Airfoil lifting force)
http://www.ef-uk.net/data/wcl.htm (Wing Cube Loading Calc) Thanks, Larry!
http://www.flyrc.com/calculator.shtml (Wing loading calculator) Thanks, dk aero!
http://www.grc.nasa.gov/WWW/k-12/airplane/short.html (NASA’s Beginners Guide to Aerodynamics) Thanks, Steve!
http://www.mh-aerotools.de/airfoils/index.htm (Aerodynamics for model aircraft, including airfoils. Large section on flying wings)
http://www.profili2.com/eng/default.htm (Airfoil plotting program)
http://regenpress.com/ (Wings and Lift Generation) Thanks, Steve!
http://www.rexresearch.com/klinfogl/klinfogl.htm#ultim (Kline/Folleman KF Airfoil)
http://sky.prohosting.com/air2/index2.htm (Model aerodynamics explained, in simple terms)
http://tracfoil.free.fr/airfoils/indexE.html (Sailplane airfoils, Free)
http://en.wikipedia.org/wiki/Longitu…atic_stability (Longitudinal Static Stability)
http://worldofkrauss.com/ (AID, Airfoil Investigation Database, Free) Thanks, DKNgyuen!
Books
http://www.amazon.com/Model-Aircraft…/dp/1854861905 (Martin Simons; Model Aircraft Aerodynamics)
http://www.amazon.com/Basics-Model-A…/dp/0911295402 (Andy Lennon; Basics of R/C Model Aircraft Design)
http://www.amazon.com/Theory-Wing-Se…ref=pd_sim_b_2 (Ira H. Abbott + A.E. von Doenhoff; Theory of Wing Sections)
http://www.amazon.com/RCadvisors-Mod…ref=pd_sim_b_2 (Carlos Reyes; RCadvisor’s Model Airplane Design Made Easy)
Note; This link contains lift information which is disputed and many believe to be inaccurate. For a further description, go here;
http://www.grc.nasa.gov/WWW/K-12/airplane/bernnew.html
http://regenpress.com/
And here;
http://www.aviation-history.com/theory/lift.htm
کتاب معروف Airplane Aerodynamics and Performance اثر دکتر رسکام .
صفحات : ۷۵۰
حجم : ۳۰ MB
Airplane Aerodynamics and Performance
http://depositfiles.com/en/files/vgqq39rro
لینک مستقیم : (برای مدت محدودی فعال است)
http://s83.eu.rapidbaz.com/get/_9Oqj/AIRPLANE_AERODYNAMICS.rar
USAF Stability & Control DATCOM
مجموعه کتب DATCOM که در ۹ جلد ارائه شده نتایج کار گروهی از متخصصین شرکت مک داگلاس آمریکا است که تحت یک قرارداد با ناسا به انجام رسیده ، هدف از ارئه این کتاب ، ارائه روش های خلاصه و سیستماتیکی است که بوسیله انها میتوان مشتقات یا ضرایب اصلی کنترل و پایداری هواپیما را بدست اورد .
این مجموعه درسال ۱۹۶۰ انتشار یافت و در سال ۱۹۷۸ مجداد با اصلاحاتی و تغییراتی به چاپ رسد ، نسخه موجود آخرین نسخه که همان ۱۹۷۸ است
کتاب ۹ جلدی به شرح زیر:
۱- جلد اول: راهنمای کتاب و خلاصه فرمولها
۲- جلد دوم: اطلاعات عمومی
۳-جلد سوم: اثرات اشیاء خارجی حمل شده توسط هواپیما مانند موشک و بمب و.. بر لیفت و دراگ و ممانها
۴-جلد چهارم: در مورد اثرات زاویه حمله
۵-جلد پنجم: اثرات زاویه سرش جانبی
۶-جلد ششم: اثرات برافزا ها و سطوح کنترل
۷-جلد هفتم: مشتقات پایداری
۸-جلد هشتم: جرم و ممان اینرسی
۹-جلد نهم: درباره هواپیماهای عمود پرواز و کوتاه برخاست(از صفخه ۲۹۶۱الی آخر)که خودم دربدر مطلب در این باره بودم.
مهمترین قسمت این مجموعه ، جلد ۷ ان است که روش های محاسبه ضرایب پایداری را ارئه کرده است . البته قسمت های مهمی همچون محاسبه ضریب Cd0و پسا و … در جلد ۴ فصلهای ۵ و ۶ و ۷ .
دانلود به صورت یک تکه : ۱۰۷٫۹۱ MB
http://ifile.it/bgqcd63/usaf_datcom.rar
پوسته ی پانوراما ساخته شده توسط Themocracy و آماده شده برای وردپرس فارسی توسط فرزاد ساغرچی
