A Tabulation Of Wind Tunnel Pressure Data And Section Aerodynamic Characteristics At Mach Numbers Of 161 And 201 For Two Trapezoidal And Three Delta Wings Having Different Surface Shapes

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.49/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.12/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Frederick Cyril Grant
Publisher :
ISBN 13 :
Total Pages : 196 pages
Book Rating : 4.05/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data at Mach Numbers of 1.61 and 2.01 of Five Swept Wings of the Same Plan Form But Different Surface Shapes written by Frederick Cyril Grant and published by . This book was released on 1958 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.80/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for a Reflex Cambered Wing and a Cambered and Twisted Wing Having the Same Swept Planform written by Emma Jean Landrum and published by . This book was released on 1962 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Julio Chu
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.96/5 ( download)

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Download or read book Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges written by Julio Chu and published by . This book was released on 1996 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Arnold S. Collier
Publisher :
ISBN 13 :
Total Pages : 254 pages
Book Rating : 4.36/5 ( download)

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Download or read book Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2, 3 and 4 (WTR1421) written by Arnold S. Collier and published by . This book was released on 1986 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Robert S. Osborne
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.25/5 ( download)

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Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.37/5 ( download)

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Download or read book A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Julio Chu
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.29/5 ( download)

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Download or read book Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges written by Julio Chu and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Peter T. Bernot
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.44/5 ( download)

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Download or read book Pressure Distributions on Blunt-delta Wings at Angles of Attack Up to 90 Degrees and Mach Number of 6.85 written by Peter T. Bernot and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: