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نمایش مورد 1-10 از 70 نتیجه جستجو شده.
عملیات
NACA-TN-1468 : Low-speed static stability and damping-in-roll characteristics of some swept and unswept low-aspect-ratio wings
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
JAN-A-465 : ACID, ACETIC (FOR ORDNANCE USE)
سازمان:
ARMY - AR - US Army Research Devlp & Engr Command, Armament Research Devlp & Engr Center
زبان:
English
سال:
1947
قیمت: 55000 تومان
JAN-A-459 : ACETIC ANHYDRIDE (FOR ORDNANCE USE)
سازمان:
ARMY - AR - US Army Research Devlp & Engr Command, Armament Research Devlp & Engr Center
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-RM-L7G31 : Lateral stability and control characteristics of an airplane model having 42.8 degrees sweptback circular-arc wing with aspect ratio 4.00, taper ratio 0.50, and sweptback tail surfaces
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-TN-1278 : Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degrees, 42 degrees and 62 degrees sweepback
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-RM-A7F06 : An investigation at low speed of a large-scale triangular wing of aspect ratio two - I. characteristics of a wing having a double-wedge airfoil section with maximum thickness at 20-percent chord
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA REPORT 874 : A Simplified Method of Elastic Stability Analysis for Thin Cylindrical Shells
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-TN-1197 : Some investigations of the general instability of stiffened metal cylinders VIII - stiffened metal cylinders subjected to pure torsion
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-TN-1341 : A simplified method of elastic-stability analysis for thin cylindrical shells I : Donnell's equation
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان
NACA-TN-1248 : Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wing
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1947
قیمت: 55000 تومان