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Author : Richard E. Kuhn,Andrew L. Byrnes
Publisher : Unknown
Page : 50 pages
File Size : 54,8 Mb
Release : 1955
Category : Aerodynamic load
ISBN : UOM:39015086490185
Author : Edward C. Polhamus
Publisher : Unknown
Page : 34 pages
File Size : 45,8 Mb
Release : 1955
Category : Airplanes
ISBN : UOM:39015095100924
Author : Arthur L. Jones,Robert M. Sorenson,Elizabeth E. Lindler
Publisher : Unknown
Page : 78 pages
File Size : 55,7 Mb
Release : 1949
Category : Aerofoils
ISBN : UOM:39015086494054
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.
Author : Arthur Leslie Jones,Alberta Alksne
Publisher : Unknown
Page : 72 pages
File Size : 52,5 Mb
Release : 1949
Category : Aerodynamics, Supersonic
ISBN : UOM:39015086493700
The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.
Author : Edward C. Polhamus
Publisher : Unknown
Page : 90 pages
File Size : 55,5 Mb
Release : 1955
Category : Aerodynamics
ISBN : UOM:39015086465732
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
Author : Edward Charles Polhamus,William C. Sleeman
Publisher : Unknown
Page : 86 pages
File Size : 54,5 Mb
Release : 1960
Category : Aerodynamics, Transonic
ISBN : UIUC:30112106588194
Author : Arthur L. Jones,John R. Spreiter,Alberta Alksne
Publisher : Unknown
Page : 644 pages
File Size : 52,7 Mb
Release : 1948
Category : Aerodynamics, Supersonic
ISBN : STANFORD:36105024795648
The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
Author : Cornelius Driver
Publisher : Unknown
Page : 58 pages
File Size : 49,9 Mb
Release : 1959
Category : Aerodynamic measurements
ISBN : UIUC:30112104505323
Author : Gerald V. Foster
Publisher : Unknown
Page : 30 pages
File Size : 54,8 Mb
Release : 1959
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112104505430
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1200 pages
File Size : 52,7 Mb
Release : 1954
Category : Aeronautics
ISBN : UOM:39015036314527
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : Anonim
Publisher : Unknown
Page : 746 pages
File Size : 40,9 Mb
Release : 194?
Category : Aeronautics
ISBN : UFL:31262081528761
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Author : Anonim
Publisher : Unknown
Page : 420 pages
File Size : 46,7 Mb
Release : 1987
Category : Astronautics
ISBN : MINN:31951000586824Q
Author : Anonim
Publisher : Unknown
Page : 940 pages
File Size : 47,5 Mb
Release : 1940
Category : Airplanes
ISBN : UOM:39015080009585
Author : Honghai Liu,Zhouping Yin,Lianqing Liu,Li Jiang,Guoying Gu,Xinyu Wu,Weihong Ren
Publisher : Springer Nature
Page : 813 pages
File Size : 47,5 Mb
Release : 2022-08-03
Category : Computers
ISBN : 9783031138225
The 4-volume set LNAI 13455 - 13458 constitutes the proceedings of the 15th International Conference on Intelligent Robotics and Applications, ICIRA 2022, which took place in Harbin China, during August 2022. The 284 papers included in these proceedings were carefully reviewed and selected from 442 submissions. They were organized in topical sections as follows: Robotics, Mechatronics, Applications, Robotic Machining, Medical Engineering, Soft and Hybrid Robots, Human-robot Collaboration, Machine Intelligence, and Human Robot Interaction.
Author : William R. Campbell
Publisher : Unknown
Page : 690 pages
File Size : 52,9 Mb
Release : 1948
Category : Strain gages
ISBN : STANFORD:36105024795614
Tests were made to determine the important performance characteristics for six types of bakelite-bonded wire strain gages commercially available and in current use by the aircraft industry. Results on the following characteristics are presented: (1) uniformity of calibration factors for individual gages of the same type, (2) variation of calibration factor with temperature, (3) creep, (4) effect of current on gage resistance, and (5) variation of gage resistance with temperature.