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Base Pressure Coefficients Obtained From The X 15 Airplane For Mach Numbers Up To 6
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Book Synopsis Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 by : Edwin J. Saltzman
Download or read book Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 written by Edwin J. Saltzman and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 by : Edwin J. Saltzman
Download or read book Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 written by Edwin J. Saltzman and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 by : Edwin J. Saltzman
Download or read book Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 written by Edwin J. Saltzman and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Base pressure measurements were made on the fuselage, 10 degree-wedge vertical fin, and side fairing of the X-15 airplane. Data are presented for Mach numbers between 1.1 and 3.2 for both powered and unpowered flight. Comparisons are made with data from small-scale-model tests, semiempirical estimates, and theory. The results of this preliminary study show that operation of the interim rocket engines reduces the base drag of the X-15 by 25 to 35% throughout the test Mach number range. Values of base drag coefficient for the side fairing and fuselage obtained from X-15 wind-tunnel models were adequate for predicting the over-all full-scale performance of the test airplane. The leading-edge sweep of the upper movable vertical fin was not an important factor affecting the fin base pressure. The power-off base pressure coefficients of the upper movable vertical fin are in general agreement with the small-scale blunt-trailing-edge-wing data of several investigators and with two-dimensional t eory. (Author).
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis X-15 Research Results by : Wendell H. Stillwell
Download or read book X-15 Research Results written by Wendell H. Stillwell and published by . This book was released on 1965 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamics of Large-angle Cones by : James F. Campbell
Download or read book Supersonic Aerodynamics of Large-angle Cones written by James F. Campbell and published by . This book was released on 1968 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Reassessment of Heavy-Duty Truck Aerodynamic Design Features and Priorities by : Edwin J. Saltzman
Download or read book A Reassessment of Heavy-Duty Truck Aerodynamic Design Features and Priorities written by Edwin J. Saltzman and published by . This book was released on 1999 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Pressure Distributions on the Vertical Stabilizers and Speed Brakes of the X-15 Airplane at Mach Numbers from 1 to 6 by : Jon S. Pyle
Download or read book Flight Pressure Distributions on the Vertical Stabilizers and Speed Brakes of the X-15 Airplane at Mach Numbers from 1 to 6 written by Jon S. Pyle and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0 by : Sheryll Goecke Powers
Download or read book Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0 written by Sheryll Goecke Powers and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1980 with total page 1284 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 with total page 1284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight-measured Base Pressure Coefficients for Thick Boundary-layer Flow Over an Aft-facing Step for Mach Numbers from 0.4 to 2.5 by : Sheryll A. Goecke
Download or read book Flight-measured Base Pressure Coefficients for Thick Boundary-layer Flow Over an Aft-facing Step for Mach Numbers from 0.4 to 2.5 written by Sheryll A. Goecke and published by . This book was released on 1973 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Drag Characteristics Obtained from Several Configurations of the Modified X-15-2 Airplane Up to Mach 6.7 by : Lawrence C. Montoya
Download or read book Drag Characteristics Obtained from Several Configurations of the Modified X-15-2 Airplane Up to Mach 6.7 written by Lawrence C. Montoya and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Force and Pressure Tests of Rocket-engine Nozzle Extensions on the 0.0667-scale X-15-2 Model at Supersonic and Hypersonic Speeds by : Earl J. Montoya
Download or read book Wind-tunnel Force and Pressure Tests of Rocket-engine Nozzle Extensions on the 0.0667-scale X-15-2 Model at Supersonic and Hypersonic Speeds written by Earl J. Montoya and published by . This book was released on 1969 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comparison of Flight Pressure Measurements with Wind-tunnel Data and Theory for the Forward Fuselage of the X-15 Airplane at Mach Numbers from 0.8 to 6.0 by : Jon S. Pyle
Download or read book Comparison of Flight Pressure Measurements with Wind-tunnel Data and Theory for the Forward Fuselage of the X-15 Airplane at Mach Numbers from 0.8 to 6.0 written by Jon S. Pyle and published by . This book was released on 1964 with total page 40 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 1969 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1961 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt: