11![Fluid mechanics / Aerodynamics / Shock wave / Blast wave / Overpressure / Speed of sound / Wave / Mach number / Wind wave / Fluid dynamics / Physics / Dynamics Fluid mechanics / Aerodynamics / Shock wave / Blast wave / Overpressure / Speed of sound / Wave / Mach number / Wind wave / Fluid dynamics / Physics / Dynamics](/pdf-icon.png) | Add to Reading ListSource URL: www.fourmilab.chLanguage: English - Date: 2012-05-24 17:30:18
|
---|
12![CHAM Limited Pioneering CFD Software for Education & Industry CFD Modelling of LPG dispersion Demonstration example The following describes the numerical analysis of the dispersion of gas release from an LPG CHAM Limited Pioneering CFD Software for Education & Industry CFD Modelling of LPG dispersion Demonstration example The following describes the numerical analysis of the dispersion of gas release from an LPG](https://www.pdfsearch.io/img/975b7ef60156c0326ee72efae13538dd.jpg) | Add to Reading ListSource URL: www.cham.co.ukLanguage: English - Date: 2012-02-08 04:44:36
|
---|
13![PV-WAVE 10.5 Release Notes February 2015 This file, PV-WAVE105_Release_Notes.pdf, contains a summary of technical changes that make PVWAVE Versions 10.5, 10.1, 10.0a and 10.0 different from previous versions. For conveni PV-WAVE 10.5 Release Notes February 2015 This file, PV-WAVE105_Release_Notes.pdf, contains a summary of technical changes that make PVWAVE Versions 10.5, 10.1, 10.0a and 10.0 different from previous versions. For conveni](https://www.pdfsearch.io/img/f182f3a59a56ce0187d169840e8bd08c.jpg) | Add to Reading ListSource URL: docs.roguewave.comLanguage: English - Date: 2015-02-17 11:38:54
|
---|
14![Afshar Explained Neil J. Gunther, M.Sc., Ph.D. Performance Dynamics Company [removed] Created March 4, 2005 Updated June 5, 2005 Afshar Explained Neil J. Gunther, M.Sc., Ph.D. Performance Dynamics Company [removed] Created March 4, 2005 Updated June 5, 2005](https://www.pdfsearch.io/img/2eb5252f89d01d6046d5f8d4c0740d7e.jpg) | Add to Reading ListSource URL: www.neilgunther.comLanguage: English - Date: 2008-10-15 09:49:19
|
---|
15![TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens, TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,](https://www.pdfsearch.io/img/7d7c0e237f913fa54bf0a0b40bd09008.jpg) | Add to Reading ListSource URL: www.logbookmag.comLanguage: English - Date: 2012-02-24 02:11:55
|
---|
16![Technical series Lowering rocket drag Rocketeers launching from Sea-level live at the bottom of a dense sea of air. This trite statement has serious consequences for rocketry however: Aerodynamic drag is the major force Technical series Lowering rocket drag Rocketeers launching from Sea-level live at the bottom of a dense sea of air. This trite statement has serious consequences for rocketry however: Aerodynamic drag is the major force](https://www.pdfsearch.io/img/d5134cf2be7c130058162203c22cb86d.jpg) | Add to Reading ListSource URL: myweb.tiscali.co.ukLanguage: English - Date: 2010-01-19 09:42:52
|
---|
17![J. Fluid Mech[removed]), vol. 750, pp. 385_400. c Cambridge University Press 2014 doi:[removed]jfm[removed]Dynamic transition from Mach to regular reflection of shock waves in a steady flow K. Naidoo1 and B. W. Skews2,† J. Fluid Mech[removed]), vol. 750, pp. 385_400. c Cambridge University Press 2014 doi:[removed]jfm[removed]Dynamic transition from Mach to regular reflection of shock waves in a steady flow K. Naidoo1 and B. W. Skews2,†](https://www.pdfsearch.io/img/268eb9a8ab73ca10b9900aeeec0becea.jpg) | Add to Reading ListSource URL: researchspace.csir.co.zaLanguage: English - Date: 2014-12-03 16:55:15
|
---|
18![THREE-DIMENSIONAL, SHOCK-ON-SHOCK INTERACTION PROBLEM* By Paul Kutler NASA Ames Research Center and Leonidas Sakell THREE-DIMENSIONAL, SHOCK-ON-SHOCK INTERACTION PROBLEM* By Paul Kutler NASA Ames Research Center and Leonidas Sakell](https://www.pdfsearch.io/img/48f86d6eea424779c9d6963e1355636f.jpg) | Add to Reading ListSource URL: history.arc.nasa.govLanguage: English - Date: 2014-06-16 15:21:25
|
---|
19![564 AIAA JOURNAL VOL. 16, NO. 6 564 AIAA JOURNAL VOL. 16, NO. 6](https://www.pdfsearch.io/img/14c4aa6e33730cfb1488d058423c8bf2.jpg) | Add to Reading ListSource URL: history.arc.nasa.govLanguage: English - Date: 2014-06-16 15:21:24
|
---|
20![COMPARISONS OF COMPUTED AND EXPERIMENTAL PRESSURES FOR TRANSONIC FLOWS ABOUT ISOLATED WINGS AND WING-FUSELAGE CONFIGURATIONS -: . By F. R. -Bailey NASA Ames Research Center COMPARISONS OF COMPUTED AND EXPERIMENTAL PRESSURES FOR TRANSONIC FLOWS ABOUT ISOLATED WINGS AND WING-FUSELAGE CONFIGURATIONS -: . By F. R. -Bailey NASA Ames Research Center](https://www.pdfsearch.io/img/512be7500f4aab1a1f155a2bfefabd96.jpg) | Add to Reading ListSource URL: history.arc.nasa.govLanguage: English - Date: 2014-06-16 15:21:24
|
---|