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Free Flight Measurements Of The Static And Dynamic Stability And Drag Of A 10 Degree Blunted Cone At Mach Numbers 35 And 85
Download Free Flight Measurements Of The Static And Dynamic Stability And Drag Of A 10 Degree Blunted Cone At Mach Numbers 35 And 85 full books in PDF, epub, and Kindle. Read online Free Flight Measurements Of The Static And Dynamic Stability And Drag Of A 10 Degree Blunted Cone At Mach Numbers 35 And 85 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10° Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10° Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurement of Drag and Static Stability for a Blunt-nosed 10° Half-angle Cone at Mach Number 15 by : Dale L. Compton
Download or read book Free-flight Measurement of Drag and Static Stability for a Blunt-nosed 10° Half-angle Cone at Mach Number 15 written by Dale L. Compton and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone by : William R. Wehrend
Download or read book Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone written by William R. Wehrend and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Stability and Drag of a Pointed and a Blunted 30 ̊half-angle Cone at Mach Numbers from 11.5 to 34 in Air by : Peter F. Intrieri
Download or read book Experimental Stability and Drag of a Pointed and a Blunted 30 ̊half-angle Cone at Mach Numbers from 11.5 to 34 in Air written by Peter F. Intrieri and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Static Stability Measurements of Cones in Hypersonic Flow by : Kurt R. Enkenhus
Download or read book Free-flight Static Stability Measurements of Cones in Hypersonic Flow written by Kurt R. Enkenhus and published by . This book was released on 1970 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Stability and Drag of a Pointed and a Blunted 30 Degrees Half-angle Cone at Mach Numbers from 11.5 to 34 in Air by : Peter F. Intrieri
Download or read book Experimental Stability and Drag of a Pointed and a Blunted 30 Degrees Half-angle Cone at Mach Numbers from 11.5 to 34 in Air written by Peter F. Intrieri and published by . This book was released on 1966 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane
Download or read book Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 written by Lucille C. Coltrane and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane
Download or read book Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 written by Lucille C. Coltrane and published by . This book was released on 1962 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Download or read book Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium written by Melvin J. Fohrman and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evaluation of Critical Sting Length on a 7-deg Cone as Determined by Measurements of Dynamic Stability Derivatives and Base Pressure for Mach Numbers 0.2 Through 1.3 by : Frederick B. Cyran
Download or read book Evaluation of Critical Sting Length on a 7-deg Cone as Determined by Measurements of Dynamic Stability Derivatives and Base Pressure for Mach Numbers 0.2 Through 1.3 written by Frederick B. Cyran and published by . This book was released on 1981 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel tests were conducted to provide sting-support interference information for planning and directing wind tunnel tests at subsonic and transonic Mach numbers. Sting-length effects on dynamic stability derivatives, static pitching moment, and base pressure of a blunt, flat-base 7- deg cone were investigated at Mach numbers 0.2 to 1.3 in the Arnold Engineering Development Center (AEDC) Propulsion Wind Tunnel Facility (PWT). Two frequencies of oscillation, nominally 5.3 and 2.9 Hz, were investigated. The boundary-layer state at the model base was turbulent for all Mach numbers greater than 0.2. The interference effects of two types of model-wake splitter plates were also investigated. The results showed that the critical sting length depended on the Mach number, angle of attack, and type of data used as the interference indicator. A critical sting length of three model diameters was determined to be suitable for all test conditions for the ratio of sting-diameter-to-model-base- diameter (0.22) for this test.
Book Synopsis Free-flight Cone Dynamic Stability Testing at High Amplitudes of Oscillation by : Bain Dayman
Download or read book Free-flight Cone Dynamic Stability Testing at High Amplitudes of Oscillation written by Bain Dayman and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of the Static and Dynamic Stability of a 0.1 Bluntness 10deg Semi Angle Cone at 90deg Angle of Attack at Mach 6.85 by : R. A. East
Download or read book Measurements of the Static and Dynamic Stability of a 0.1 Bluntness 10deg Semi Angle Cone at 90deg Angle of Attack at Mach 6.85 written by R. A. East and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Investigation of the Aerodynamic Characteristics of a 10-deg Semiangle Cone at Mach Numbers from 6 to 16 by : Clement J. Welsh
Download or read book Free-flight Investigation of the Aerodynamic Characteristics of a 10-deg Semiangle Cone at Mach Numbers from 6 to 16 written by Clement J. Welsh and published by . This book was released on 1969 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 1000-ft hypervelocity range was used to obtain the free-flight static and dynamic stability and drag data presented for a 10-deg semiangle cone. Measurements indicate that the damping-in-pitch derivatives for the cone increase appreciably with increasing Mach number between M = 8 and 16 at a Reynolds number (based on model length and free-stream conditions) of about 400,000. Further, the pitching-moment derivative for the cone decreases significantly as the nose-radius to base-radius ratio of the cone is increased up to 0.1 for amplitudes greater than about 5 deg. Comparisons of the range stability data with wind tunnel data (involving sting-supported models) obtained in different test facilities indicate that appreciable differences in the pitching-moment derivative and the damping-in-pitch derivatives exist in some cases. (Author).
Book Synopsis Aerodynamic Characteristics of a Large-angle Blunt Cone with and Without Fence-type Afterbodies by : Kenneth W. McAlister
Download or read book Aerodynamic Characteristics of a Large-angle Blunt Cone with and Without Fence-type Afterbodies written by Kenneth W. McAlister and published by . This book was released on 1971 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations by : C. J. Welsh
Download or read book Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations written by C. J. Welsh and published by . This book was released on 1972 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly blunted 10-deg semiangle cones with and without ablation occurring on the conical skirts. The configurations investigated included ones having fore- and aft-positioned ablation sleeves, as well as one with a skirt material which did not ablate. The investigation was conducted for a Mach number near 14 and a Reynolds number, based on cone length and free-stream conditions, of about 55000.
