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Wind Tunnel Force Measurements On A 1 20 Scale Model Of Black Arrow At Mach Numbers Of 12 15 And 20
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Book Synopsis Wind-tunnel Force Measurements on a 1/20 Scale Model of Black Arrow at Mach Numbers of 1.2, 1.5 and 2.0 by : J. R. Hall
Download or read book Wind-tunnel Force Measurements on a 1/20 Scale Model of Black Arrow at Mach Numbers of 1.2, 1.5 and 2.0 written by J. R. Hall and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Force Measurements on a .05 Scale Model of Black Arrow at Mach Numbers of 1.2, 1.5 and 2.0 by : J. R. Hall
Download or read book Wind-tunnel Force Measurements on a .05 Scale Model of Black Arrow at Mach Numbers of 1.2, 1.5 and 2.0 written by J. R. Hall and published by . This book was released on 1973 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 854 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Aeronautical Journal written by and published by . This book was released on 1974 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of the Model Blockage for Wind Tunnels at Mach Numbers 1.5 to 19.5 by : C. J. Schueler
Download or read book An Investigation of the Model Blockage for Wind Tunnels at Mach Numbers 1.5 to 19.5 written by C. J. Schueler and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the test section flow blockage characteristics was conducted in the 12- by 12 inch supersonic wind tunnel (Tunnel E-1) of the Von Karman Gas Dynamics Facility (AEDC). The purpose of the tests was to determine whether a method of predicting the maximum size model which will permit the establishment of supersonic flow, based on the model frontal area and bow shock-wave strength, is applicable over a wide range of Mach numbers. The tests conducted over the Mach number range from 1.5 to 5 using test models consisting of 15, 20, and 20 degrees half-angle cones, cone-cylinder combinations, and a series of discs. The inadequacy of the one dimensional, normal shock theory for predicting allowable model sizes was reconfirmed in these tests. Furthermore a correlation based on shock wave strength and model frontal area was found to be suitable only over a limited range of Mach numbers. Permissible hemisphere-cylinder model sizes from several wind tunnels covering the Mach number range from 1.5 to 19.5 are also presented.
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1974 with total page 1088 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 1074 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster by : Albin O. Pearson
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster written by Albin O. Pearson and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of the Fin Loads of a 1/8-scale Model Simulating the First Stage of the Scout Research Vehicle by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of the Fin Loads of a 1/8-scale Model Simulating the First Stage of the Scout Research Vehicle written by Thomas C. Kelly and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1974 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Measurements of Aerodynamic Damping Derivatives of a Launch Vehicle Vibrating in Free-free Bending Modes at Mach Numbers from 0.70 to 2.87 and Comparisons with Theory by : Perry W. Hanson
Download or read book Wind Tunnel Measurements of Aerodynamic Damping Derivatives of a Launch Vehicle Vibrating in Free-free Bending Modes at Mach Numbers from 0.70 to 2.87 and Comparisons with Theory written by Perry W. Hanson and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50 by : Neil Arthur Zarin
Download or read book Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50 written by Neil Arthur Zarin and published by . This book was released on 1964 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Force Measurements on Axisymmetric Models with Hammerhead Noses at Transonic Speeds by : Bruno J. Gambucci
Download or read book Force Measurements on Axisymmetric Models with Hammerhead Noses at Transonic Speeds written by Bruno J. Gambucci and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule by : Albin O. Pearson
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule written by Albin O. Pearson and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method to Calculate Uncertainties of Drag Coefficient Wind Tunnel Data by : Spence E. Peters (Jr.)
Download or read book A Method to Calculate Uncertainties of Drag Coefficient Wind Tunnel Data written by Spence E. Peters (Jr.) and published by . This book was released on 1980 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1974 with total page 1176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
