Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers
Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple nume...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Report |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | Martin,Fred W Purvis,James Burkhalter,John E Martin,Brent D |
| description | Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple numerical method is presented and compared with both experimental results and the results of other analytical methods for potential flow. (Author) |
| format | Report |
| fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA050267</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA050267</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA0502673</originalsourceid><addsrcrecordid>eNqFjTEKwkAQRdNYiHoDi7mAEBS1XmJEC220l83urBnY7IaZjZAjeGtjsLf68P_j_Wn2VkH7XkhABwtFbFrNJDFAdHDDF7L2cMFURyvgIo9Elyg8QSFH2wfdkBlbRhGqyFPqR9c5JGSHjMEglM6hSQJdCylCwZTIfM3a1HDtmgpZ5tnEaS-4-OUsWx7Le3Fa2YF9yPCJ6aEOKt_m691-82f-ABadSYE</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers</title><source>DTIC Technical Reports</source><creator>Martin,Fred W ; Purvis,James ; Burkhalter,John E ; Martin,Brent D</creator><creatorcontrib>Martin,Fred W ; Purvis,James ; Burkhalter,John E ; Martin,Brent D ; AUBURN UNIV ALA DEPT OF AEROSPACE ENGINEERING</creatorcontrib><description>Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple numerical method is presented and compared with both experimental results and the results of other analytical methods for potential flow. (Author)</description><language>eng</language><subject>AERODYNAMIC CHARACTERISTICS ; AERODYNAMIC CONFIGURATIONS ; AERODYNAMIC FORCES ; APPROXIMATION(MATHEMATICS) ; ASYMPTOTIC SERIES ; BOUNDARY LAYER FLOW ; COMPRESSIBLE FLOW ; EXTERNAL STORES ; FAR FIELD ; FINITE ELEMENT ANALYSIS ; Fluid Mechanics ; INTERFERENCE ; INVISCID FLOW ; MATHEMATICAL MODELS ; NONLINEAR DIFFERENTIAL EQUATIONS ; Numerical Mathematics ; NUMERICAL METHODS AND PROCEDURES ; PE62602F ; PERTURBATIONS ; POTENTIAL FLOW ; PRESSURE DISTRIBUTION ; SHOCK WAVES ; SLENDER BODIES ; TRANSONIC FLOW ; WUAFATL25670215</subject><creationdate>1977</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA050267$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Martin,Fred W</creatorcontrib><creatorcontrib>Purvis,James</creatorcontrib><creatorcontrib>Burkhalter,John E</creatorcontrib><creatorcontrib>Martin,Brent D</creatorcontrib><creatorcontrib>AUBURN UNIV ALA DEPT OF AEROSPACE ENGINEERING</creatorcontrib><title>Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers</title><description>Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple numerical method is presented and compared with both experimental results and the results of other analytical methods for potential flow. (Author)</description><subject>AERODYNAMIC CHARACTERISTICS</subject><subject>AERODYNAMIC CONFIGURATIONS</subject><subject>AERODYNAMIC FORCES</subject><subject>APPROXIMATION(MATHEMATICS)</subject><subject>ASYMPTOTIC SERIES</subject><subject>BOUNDARY LAYER FLOW</subject><subject>COMPRESSIBLE FLOW</subject><subject>EXTERNAL STORES</subject><subject>FAR FIELD</subject><subject>FINITE ELEMENT ANALYSIS</subject><subject>Fluid Mechanics</subject><subject>INTERFERENCE</subject><subject>INVISCID FLOW</subject><subject>MATHEMATICAL MODELS</subject><subject>NONLINEAR DIFFERENTIAL EQUATIONS</subject><subject>Numerical Mathematics</subject><subject>NUMERICAL METHODS AND PROCEDURES</subject><subject>PE62602F</subject><subject>PERTURBATIONS</subject><subject>POTENTIAL FLOW</subject><subject>PRESSURE DISTRIBUTION</subject><subject>SHOCK WAVES</subject><subject>SLENDER BODIES</subject><subject>TRANSONIC FLOW</subject><subject>WUAFATL25670215</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1977</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjTEKwkAQRdNYiHoDi7mAEBS1XmJEC220l83urBnY7IaZjZAjeGtjsLf68P_j_Wn2VkH7XkhABwtFbFrNJDFAdHDDF7L2cMFURyvgIo9Elyg8QSFH2wfdkBlbRhGqyFPqR9c5JGSHjMEglM6hSQJdCylCwZTIfM3a1HDtmgpZ5tnEaS-4-OUsWx7Le3Fa2YF9yPCJ6aEOKt_m691-82f-ABadSYE</recordid><startdate>197709</startdate><enddate>197709</enddate><creator>Martin,Fred W</creator><creator>Purvis,James</creator><creator>Burkhalter,John E</creator><creator>Martin,Brent D</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197709</creationdate><title>Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers</title><author>Martin,Fred W ; Purvis,James ; Burkhalter,John E ; Martin,Brent D</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA0502673</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1977</creationdate><topic>AERODYNAMIC CHARACTERISTICS</topic><topic>AERODYNAMIC CONFIGURATIONS</topic><topic>AERODYNAMIC FORCES</topic><topic>APPROXIMATION(MATHEMATICS)</topic><topic>ASYMPTOTIC SERIES</topic><topic>BOUNDARY LAYER FLOW</topic><topic>COMPRESSIBLE FLOW</topic><topic>EXTERNAL STORES</topic><topic>FAR FIELD</topic><topic>FINITE ELEMENT ANALYSIS</topic><topic>Fluid Mechanics</topic><topic>INTERFERENCE</topic><topic>INVISCID FLOW</topic><topic>MATHEMATICAL MODELS</topic><topic>NONLINEAR DIFFERENTIAL EQUATIONS</topic><topic>Numerical Mathematics</topic><topic>NUMERICAL METHODS AND PROCEDURES</topic><topic>PE62602F</topic><topic>PERTURBATIONS</topic><topic>POTENTIAL FLOW</topic><topic>PRESSURE DISTRIBUTION</topic><topic>SHOCK WAVES</topic><topic>SLENDER BODIES</topic><topic>TRANSONIC FLOW</topic><topic>WUAFATL25670215</topic><toplevel>online_resources</toplevel><creatorcontrib>Martin,Fred W</creatorcontrib><creatorcontrib>Purvis,James</creatorcontrib><creatorcontrib>Burkhalter,John E</creatorcontrib><creatorcontrib>Martin,Brent D</creatorcontrib><creatorcontrib>AUBURN UNIV ALA DEPT OF AEROSPACE ENGINEERING</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Martin,Fred W</au><au>Purvis,James</au><au>Burkhalter,John E</au><au>Martin,Brent D</au><aucorp>AUBURN UNIV ALA DEPT OF AEROSPACE ENGINEERING</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers</btitle><date>1977-09</date><risdate>1977</risdate><abstract>Analytical approaches are considered which might be used to improve and extend current aerodynamic analysis to include the compressibility effects up to and including critical mach numbers. The Rayleigh-Janzen solution is considered for both small disturbance and exact potential flows. A simple numerical method is presented and compared with both experimental results and the results of other analytical methods for potential flow. (Author)</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_dtic_stinet_ADA050267 |
| source | DTIC Technical Reports |
| subjects | AERODYNAMIC CHARACTERISTICS AERODYNAMIC CONFIGURATIONS AERODYNAMIC FORCES APPROXIMATION(MATHEMATICS) ASYMPTOTIC SERIES BOUNDARY LAYER FLOW COMPRESSIBLE FLOW EXTERNAL STORES FAR FIELD FINITE ELEMENT ANALYSIS Fluid Mechanics INTERFERENCE INVISCID FLOW MATHEMATICAL MODELS NONLINEAR DIFFERENTIAL EQUATIONS Numerical Mathematics NUMERICAL METHODS AND PROCEDURES PE62602F PERTURBATIONS POTENTIAL FLOW PRESSURE DISTRIBUTION SHOCK WAVES SLENDER BODIES TRANSONIC FLOW WUAFATL25670215 |
| title | Analysis and Comparison of Several Methods for Computing Aerodynamic Compressibility and Interference Effects up to Critical Mach Numbers |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T05%3A29%3A03IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Analysis%20and%20Comparison%20of%20Several%20Methods%20for%20Computing%20Aerodynamic%20Compressibility%20and%20Interference%20Effects%20up%20to%20Critical%20Mach%20Numbers&rft.au=Martin,Fred%20W&rft.aucorp=AUBURN%20UNIV%20ALA%20DEPT%20OF%20AEROSPACE%20ENGINEERING&rft.date=1977-09&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADA050267%3C/dtic_1RU%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |