General Aviation Preliminary Structural Design in a Personal Computer Environment

The computer environment which allows the analyst to interact with a program by means of windows, dialogs, pull-down menus and check boxes is probably the most comfortable to the largest number of users. This environment is becoming available to both x-ray and electron energy loss analysts in commercial products and in programs written by analysts in the field. One such program for a personal computer has been under developement by the authors as a joint project at the NIH and the NIST. This program not only enables the analyst to process and display spectral data from electron column instruments but also provides the analyst the additional powerful capability to model the physical processes involved in the generation of an x-ray spectrum. The procedure to emulate the experimental environment and specimen to generate a series of spectra reflecting the relevant physics and statistics was previously described in some detail in terms of the application to estimating detection limits under proposed experimental conditions [1].

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Recommended standard for seismic (/radar) data files in the personal computer environment

Geophysics ◽

10.1190/1.1442942 ◽

1990 ◽

Vol 55 (9) ◽

pp. 1260-1271 ◽

Cited By ~ 7

Author(s):

S. E. Pullan

Keyword(s):

Personal Computer ◽

Data File ◽

Radar Data ◽

Small Computer ◽

File Format ◽

Shallow Seismic ◽

Computer Environment ◽

Data Files

This paper is the result of the work of a subcommittee of SEG’s Engineering and Groundwater Geophysics Committee. It recommends a data file format for raw or processed shallow seismic or digital radar data in the small computer environment. It is recommended that this format be known as the SEG-2 format.

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Image Data Compression In A Personal Computer Environment

10.1117/12.948457 ◽

1988 ◽

Author(s):

Paul M. Farrelle ◽

Daniel G. Harrington ◽

Anil K. Jain

Keyword(s):

Data Compression ◽

Personal Computer ◽

Image Data ◽

Computer Environment ◽

Image Data Compression

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A power system CAD package for the workstation and personal computer environment

IEEE Transactions on Power Systems ◽

10.1109/59.131088 ◽

1991 ◽

Vol 6 (1) ◽

pp. 400-406 ◽

Cited By ~ 11

Author(s):

N.C. Pahalawaththa ◽

C.P. Arnold ◽

M. Shurety

Keyword(s):

Power System ◽

Personal Computer ◽

Computer Environment

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Data conversion between IS&C format and DICOM format images in a personal computer environment

Proceedings of the Fourth International Conference on Image Management and Communication (IMAC 95) ◽

10.1109/imac.1995.532568 ◽

2002 ◽

Author(s):

Y. Ando ◽

O. Kawaguchi ◽

M. Kitamura ◽

K. Ogasawara ◽

A. Kubo ◽

...

Keyword(s):

Personal Computer ◽

Data Conversion ◽

Computer Environment

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A personal computer environment for realtime programming

Software Engineering Education - Lecture Notes in Computer Science ◽

10.1007/bfb0042357 ◽

2006 ◽

pp. 156-168

Author(s):

James D. Schoeffler

Keyword(s):

Personal Computer ◽

Computer Environment

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A digital signal processor based accelerator for artificial neural network simulations in a personal computer environment

1993 IEEE Instrumentation and Measurement Technology Conference ◽

10.1109/imtc.1993.382567 ◽

2002 ◽

Author(s):

A. Proctor ◽

W.B. Hudson

Keyword(s):

Neural Network ◽

Artificial Neural Network ◽

Personal Computer ◽

Digital Signal Processor ◽

Digital Signal ◽

Computer Environment ◽

Network Simulations ◽

Artificial Neural ◽

Signal Processor

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Design and static testing of wing structure of a composite four-seater electric aircraft

Science and Engineering of Composite Materials ◽

10.1515/secm-2020-0023 ◽

2020 ◽

Vol 27 (1) ◽

pp. 258-263

Author(s):

Kang Yang ◽

Yi-lin Guo ◽

Dong-hui Li ◽

Gang Ma ◽

Hao Geng ◽

...

Keyword(s):

Finite Element ◽

Structural Design ◽

Leading Edge ◽

General Aviation ◽

Civil Aviation ◽

Analysis Model ◽

Element Analysis ◽

Static Test ◽

Electric Aircraft ◽

Composite Wing

AbstractBecause of its light weight, high strength, designable, composite materials are more and more widely used in the field of aerospace, especially in the field of general aviation. In this paper, the structural design and analysis of the composite wing (include wing beam, rib, skin, leading edge and trailing edge) of a four-seater electric aircraft were carried out. The finite element numerical analysis model of the composite wing was established, and the deformation and strain distribution of the composite wing under the limited load required by airworthiness regulations were calculated. Finally, the static test of the whole composite wing was carried out to verify the accuracy of the finite element results. The finite element analysis and testing results showed that the structural design of the composite wing of the electric aircraft meets the structural strength requirements specified in the airworthiness standard (part 23 of China civil aviation regulations: air-worthiness requirements for normal, practical, special effects and commuting aircraft: CCAR 23-R3)

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