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Published 1/2024
Created by Tamir Nachum
MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz, 2 Ch
Genre: eLearning | Language: English | Duration: 13 Lectures ( 1h 7m ) | Size: 318 MB

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Published 1/2024
Created by Hamaad Masroor
MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz, 2 Ch
Genre: eLearning | Language: English | Duration: 19 Lectures ( 2h 1m ) | Size: 1.74 GB

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Published 1/2024
MP4 | Video: h264, 1920x1080 | Audio: AAC, 44.1 KHz
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Last updated 1/2020
Created by Haitham Eldalil
MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz, 2 Ch
Genre: eLearning | Language: English + srt | Duration: 11 Lectures ( 1h 43m ) | Size: 501 MB

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Published 1/2024
MP4 | Video: h264, 1920x1080 | Audio: AAC, 44.1 KHz
Language: English | Size: 535.30 MB | Duration: 1h 7m
Learn how currencies are quoted, bought and sold.

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Published 1/2024
Created by OLIVER EKLU
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Genre: eLearning | Language: English | Duration: 55 Lectures ( 5h 50m ) | Size: 2.87 GB

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Published 1/2024
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Published 1/2024
Created by SKILL MANOR
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Genre: eLearning | Language: English | Duration: 13 Lectures ( 52m ) | Size: 530 MB

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Last updated 12/2023
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Genre: eLearning | Language: English
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Free Download Basics of Aerothermodynamics by E. H. Hirschel
English | PDF (True) | 2005 | 419 Pages | ISBN : 3642060501 | 19.9 MB
The last two decades have brought two important developments for aeroth- modynamics. One is that airbreathing hypersonic flight became the topic of technology programmes and extended system studies. The other is the emergence and maturing of the discrete numerical methods of aerodyn- ics/aerothermodynamics complementary to the ground-simulation facilities, with the parallel enormous growth of computer power. Airbreathing hypersonic flight vehicles are, in contrast to aeroassisted re-entry vehicles, drag sensitive. They have, further, highly integrated lift and propulsion systems. This means that viscous eflFects, like boundary-layer development, laminar-turbulent transition, to a certain degree also strong interaction phenomena, are much more important for such vehicles than for re-entry vehicles. This holds also for the thermal state of the surface and thermal surface effects, concerning viscous and thermo-chemical phenomena (more important for re-entry vehicles) at and near the wall. The discrete numerical methods of aerodynamics/aerothermodynamics permit now - what was twenty years ago not imaginable - the simulation of high speed flows past real flight vehicle configurations with thermo-chemical and viscous effects, the description of the latter being still handicapped by in sufficient flow-physics models. The benefits of numerical simulation for flight vehicle design are enormous: much improved aerodynamic shape definition and optimization, provision of accurate and reliable aerodynamic data, and highly accurate determination of thermal and mechanical loads. Truly mul- disciplinary design and optimization methods regarding the layout of thermal protection systems, all kinds of aero-servoelasticity problems of the airframe, et cetera, begin now to emerge.