Modern helicopter design / by Eric M. Hollmann and Martin Hollmann.
نوع المادة :
نصالناشر:Monterey, Calif. : Aircraft Design, Incorporated, [2001]تاريخ حقوق النشر: ©2001وصف:1 volume (various pagings) : illustrations ; 28 cmنوع المحتوى:- text
- unmediated
- volume
- 1893639134
- 9781893639133
- TL716 .H655 2001
| نوع المادة | المكتبة الحالية | رقم الطلب | رقم النسخة | حالة | تاريخ الإستحقاق | الباركود | |
|---|---|---|---|---|---|---|---|
كتاب
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UAE Federation Library | مكتبة اتحاد الإمارات General Collection | المجموعات العامة | TL716 .H655 2001 (إستعراض الرف(يفتح أدناه)) | C.1 | Library Use Only | داخل المكتبة فقط | 30020000026247 | ||
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كتاب
|
UAE Federation Library | مكتبة اتحاد الإمارات General Collection | المجموعات العامة | TL716 .H655 2001 (إستعراض الرف(يفتح أدناه)) | C.2 | المتاح | 30020000026246 |
Browsing UAE Federation Library | مكتبة اتحاد الإمارات shelves, Shelving location: General Collection | المجموعات العامة إغلاق مستعرض الرف(يخفي مستعرض الرف)
| TL712 S52 2000 The airline training pilot / | TL712 S52 2000 The airline training pilot / | TL716 .A584 1996 The helicopter : An illustrated history of rotary-winged aircraft | TL716 .H655 2001 Modern helicopter design / | TL716 .H655 2001 Modern helicopter design / | TL716 J36 IHS Jane's helicopter markets & systems/ | TL716 J36 IHS Jane's helicopter markets & systems/ |
Includes bibliographical references.
"Describes how to design helicopters, gyroplanes and compound helicopters such as the XH-51A and the Rotordyne. Many basic computer programs that run under Windows 95/98 such as: HPERF. BAS for helicopter performance in forward flight and hover. ROTOR. BAS used for rotor blade dynamics, flapping, bending moments, airloads, rotor tilt, blade pitch for any azimuth in hover and forward flight. CHDYNAM. BAS stability program for compound helicopters and helicopters. Plot programs for airfoils: NACA 8-H-12, NACA23012, RXM13Gyro, Eppler E 361, NACA0012, RXM Stopped Rotor. PPLOT1. BAS calculates airfoil structural properties for Clark Y airfoil of any thickness. ARTROTOR. BAS determine the bending moments, deflection, centrifugal force of an articulated blade in hover. RIGROTOR. BAS bending moments, deflections, CF for rigid blades in hover. Uses finite difference method. PPERF. BAS rotor/prop performance program developed by Peter Talbot at NASA GYROPERF. BAS gyroplane performance for power required and power available plots. JUMPSTRT. BAS jump start performance for gyroplanes using a prespin system for the rotor."--Publisher's Web site.
