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Investigation Of The Asymmetric Aerodynamic Characteristics Of Cylindrical Bodies Of Revolution With Variations In Nose Geometry And Rotational Orientation At Angles Of Attack To 58and Mach Numbers To 2
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Book Synopsis 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 :
Download or read book 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 written by and published by . This book was released on 1979 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 by :
Download or read book Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 written by and published by . This book was released on 1979 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 :
Download or read book 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 written by and published by . This book was released on 1979 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Assymtric 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 : Robert L. Kruse
Download or read book Investigation of the Assymtric 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 written by Robert L. Kruse and published by . This book was released on 1979 with total page 93 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1981 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg by :
Download or read book A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg written by and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Leland Howard Jorgensen
Download or read book 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 written by Leland Howard Jorgensen and published by . This book was released on 1974 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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
Download or read book 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 written by Leland Howard Jorgensen and published by . This book was released on 1975 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber written by Barrett L. Shrout and published by . This book was released on 1983 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Asymmetric Lateral-directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack by : Paul L. Coe
Download or read book Asymmetric Lateral-directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack written by Paul L. Coe and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1974 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1975 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Two Bodies of Revolution with Noses of Varying Spherical Bluntness at Mach Numbers from 0.6 to 1.5 by : E. G Allee (Jr)
Download or read book Aerodynamic Characteristics of Two Bodies of Revolution with Noses of Varying Spherical Bluntness at Mach Numbers from 0.6 to 1.5 written by E. G Allee (Jr) and published by . This book was released on 1973 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was conducted to determine the static stability characteristics of two bodies of revolution fitted with 2-, 3-, and 4-cal tangent ogive noses of varying spherical bluntness. Testing was conducted at Mach numbers from 0.6 to 1.5 and angles of attack from -2 to 14 deg. The major effect of blunting the noses was evidenced in the axial-force coefficient. Lengthening the noses from 2 to 4 cal caused a forward movement of the center-of-pressure location and a corresponding decrease in axial-force coefficient at Mach numbers of 1.0 and higher. Changing from a 5- to a 9-cal midbody resulted in an increase in axial-force coefficient and an aft movement of the center-of-pressure location. (Author).
Book Synopsis Aerodynamic Characteristics of 2-, 3-, and 4-, Caliber Tangent-ogive Cylinders with Nose Bluffness Ratios of 0.00, 0.25, 0.50, and 0.75 at Mach Numbers from 0.6 to 4.0 by : Carroll B. Butler
Download or read book Aerodynamic Characteristics of 2-, 3-, and 4-, Caliber Tangent-ogive Cylinders with Nose Bluffness Ratios of 0.00, 0.25, 0.50, and 0.75 at Mach Numbers from 0.6 to 4.0 written by Carroll B. Butler and published by . This book was released on 1977 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report summarizes wind tunnel test data on various body alone configurations which provide a data matrix for bluff and pointed bodies of revolution with systematic variations in nose bluffness, nose fineness ratio, and cylinder afterbody fineness ratio. Modular model components were used to obtain static stability and drag data, with emphasis on the effect of nose bluffness on drag. Although data is included for tangent ogive noses of fineness ratio 2, 2.25, 2.5, 3.0, and 4, the nose fineness ratios of 2, 3, and 4 calibers include a systematic variation in nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 on cylindrical midsections of 5, 7, 9, and 11 calibers. A 1-caliber cylindrical afterbody is used with all configurations in this report.
Book Synopsis Some Effects of Nose Bluntness and Fineness Ration on the Static Longitudinal Aerodynamic Characteristics of Bodies of Revolution at Bussonic Speeds by : William C. Hayes
Download or read book Some Effects of Nose Bluntness and Fineness Ration on the Static Longitudinal Aerodynamic Characteristics of Bodies of Revolution at Bussonic Speeds written by William C. Hayes and published by . This book was released on 1961 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Book Synopsis Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 by : Harvey A. Wallskog
Download or read book Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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