Author : Leland Howard Jorgensen
Publisher : Unknown
Page : 100 pages
File Size : 55,8 Mb
Release : 1974
Category : Aerodynamics
ISBN : UIUC:30112106563700
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 book. This book definitely worth reading, it is an incredibly well-written.
NASA Technical Memorandum
Author : Anonim
Publisher : Unknown
Page : 244 pages
File Size : 40,8 Mb
Release : 1979
Category : Aeronautics
ISBN : MINN:31951000845119J
NASA Technical Memorandum by Anonim Pdf
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Author : Leland Howard Jorgensen
Publisher : Unknown
Page : 100 pages
File Size : 42,9 Mb
Release : 1975
Category : Aerodynamics
ISBN : UIUC:30112106563726
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by Leland Howard Jorgensen Pdf
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 1388 pages
File Size : 41,8 Mb
Release : 1971
Category : Government publications
ISBN : OSU:32437010622500
Monthly Catalog of United States Government Publications by Anonim Pdf
Monthly Catalog of United States Government Publications, Cumulative Index
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1408 pages
File Size : 47,7 Mb
Release : 1976
Category : United States
ISBN : STANFORD:36105021034173
Monthly Catalog of United States Government Publications, Cumulative Index by United States. Superintendent of Documents Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 1074 pages
File Size : 46,6 Mb
Release : 1979
Category : Aeronautics
ISBN : UIUC:30112075601556
Scientific and Technical Aerospace Reports by Anonim Pdf
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Author : Leland H. Jorgensen
Publisher : Unknown
Page : 122 pages
File Size : 45,5 Mb
Release : 1975
Category : Aerodynamics
ISBN : STANFORD:36105024783636
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by Leland H. Jorgensen Pdf
Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0
Author : Leland H. Jorgensen,Edgar R. Nelson
Publisher : Unknown
Page : 236 pages
File Size : 46,5 Mb
Release : 1976
Category : Aerodynamics
ISBN : STANFORD:36105024823812
Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 by Leland H. Jorgensen,Edgar R. Nelson Pdf
Government Reports Annual Index
Author : Anonim
Publisher : Unknown
Page : 882 pages
File Size : 52,5 Mb
Release : 1975
Category : Government reports announcements & index
ISBN : MINN:30000008703088
Government Reports Annual Index by Anonim Pdf
Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Author : Leland H. Jorgensen
Publisher : Unknown
Page : 164 pages
File Size : 51,6 Mb
Release : 1976
Category : Aerodynamics
ISBN : STANFORD:36105024823804
Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by Leland H. Jorgensen Pdf
Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 Degrees and Mach Numbers to 2
Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 48,7 Mb
Release : 1979
Category : Electronic
ISBN : NASA:31769000541303
Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 Degrees and Mach Numbers to 2 by Anonim Pdf
Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58ånd Mach Numbers to 2
Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 51,5 Mb
Release : 1979
Category : Aerodynamics
ISBN : UIUC:30112106660167
Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58ånd Mach Numbers to 2 by Anonim Pdf
Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0.25 to 2
Author : Anonim
Publisher : Unknown
Page : 106 pages
File Size : 52,8 Mb
Release : 1975
Category : Electronic
ISBN : NASA:31769000534480
Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0.25 to 2 by Anonim Pdf
Side Forces on Forebodies at High Angles of Attack and Mach Numbers from 0.1 to 0.7
Author : Anonim
Publisher : Unknown
Page : 148 pages
File Size : 54,5 Mb
Release : 1977
Category : Aerodynamics
ISBN : UIUC:30112106567040
Side Forces on Forebodies at High Angles of Attack and Mach Numbers from 0.1 to 0.7 by Anonim Pdf
Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7
Author : Anonim
Publisher : Unknown
Page : 120 pages
File Size : 42,6 Mb
Release : 1977
Category : Aerodynamic load
ISBN : UIUC:30112106567032