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 Author: Emma Jean Landrum Publisher: Published: 1962 Total Pages: 76 ISBN-13: DOWNLOAD EBOOK →
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 Author: Emma Jean Landrum Publisher: Published: 1962 Total Pages: 72 ISBN-13: DOWNLOAD EBOOK →
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 Author: Frederick Cyril Grant Publisher: Published: 1958 Total Pages: 196 ISBN-13: DOWNLOAD EBOOK →
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 Author: Emma Jean Landrum Publisher: Published: 1962 Total Pages: 70 ISBN-13: DOWNLOAD EBOOK →
Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges Author: Julio Chu Publisher: Published: 1996 Total Pages: 34 ISBN-13: DOWNLOAD EBOOK →
Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2, 3 and 4 (WTR1421) Author: Arnold S. Collier Publisher: Published: 1986 Total Pages: 254 ISBN-13: DOWNLOAD EBOOK →
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 Author: Robert S. Osborne Publisher: Published: 1960 Total Pages: 20 ISBN-13: DOWNLOAD EBOOK →
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 Author: Emma Jean Landrum Publisher: Published: 1962 Total Pages: 40 ISBN-13: DOWNLOAD EBOOK →
Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges Author: Julio Chu Publisher: Published: 1996 Total Pages: ISBN-13: DOWNLOAD EBOOK →
Pressure Distributions on Blunt-delta Wings at Angles of Attack Up to 90 Degrees and Mach Number of 6.85 Author: Peter T. Bernot Publisher: Published: 1963 Total Pages: 48 ISBN-13: DOWNLOAD EBOOK →