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Data Report For A Test Program To Study Transonic Flow Fields About Aircraft With Application To External Stores Volume Vi 16t Wind Tunnel Tests
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Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume VI. 16T Wind Tunnel Tests by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume VI. 16T Wind Tunnel Tests written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume VI presents data obtained for the 4-percent thick wing model in the 16T Wind Tunnel.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume I. Summary Report, Tunnel-Empty and Mach-Number Survey Data, Force and Moment Data, and Pressure Data by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume I. Summary Report, Tunnel-Empty and Mach-Number Survey Data, Force and Moment Data, and Pressure Data written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. This report presents the data obtained during the test program conducted in the 4T and 16T Wind Tunnels at Arnold Engineering Development Center. The Flow-field data were obtained at Mach numbers 0.925, 0.975, and 1.025 and constitute the major part of the data. Volume I is a summary report which gives detailed information on the test program and presents uncertainties associated with the various types of data taken in the 4T Wind Tunnel. The volume also presents tunnel-empty and Mach-number surveys, as well as tabulated force and moment and pressure data for the Mach number range 0.80 to 1.15 and angles of attack -2, -5, 0, 2, and 5.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 337 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. Volume V presents the tabulated flow-field data for 6-percent thick wing model.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume II. Mach Number 0.925 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume II. Mach Number 0.925 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 249 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume II, presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.925.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume III. Mach Number 0.975 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume III. Mach Number 0.975 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 249 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume III presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.975.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume IV. Mach Number 1.025 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume IV. Mach Number 1.025 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume IV presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 1.025.
Book Synopsis Transonic Symposium: Theory, Application, and Experiment by :
Download or read book Transonic Symposium: Theory, Application, and Experiment written by and published by . This book was released on 1989 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis TAS--a Transonic Aircraft/store Flow Field Prediction Code by : D. S. Thompson
Download or read book TAS--a Transonic Aircraft/store Flow Field Prediction Code written by D. S. Thompson and published by . This book was released on 1983 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields About Wing-Body/Pylon/Store Combinations. Volume II. Flow Field Survey Data for Configurations 21 and 22 by : S. S. Stahara
Download or read book Data Report for a Test Program to Study Transonic Flow Fields About Wing-Body/Pylon/Store Combinations. Volume II. Flow Field Survey Data for Configurations 21 and 22 written by S. S. Stahara and published by . This book was released on 1978 with total page 247 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume of the data report presents the flow-field survey data for configurations 21 and 22 at Mach numbers M1 = 0.925, M2 = 0.950, and M3 = 1.05 and angles of attack alpha = 0 deg, 2 deg, and 5 deg. The data were obtained in the 4T Wind Tunnel at Arnold Engineering and Development Center. The tests were performed at a nominal Reynolds number per foot of 3.0 million.
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 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1981 with total page 986 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2 by :
Download or read book Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2 written by and published by . This book was released on 1989 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Contractor Report written by and published by . This book was released on 1983 with total page 504 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Conference Publication written by and published by . This book was released on 1977 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind Tunnel Test to Study the Mutual Interference of Multiple Bodies in the Flow Field of the F-4C Aircraft in the Transonic Speed Range by : A. A. Hesketh
Download or read book A Wind Tunnel Test to Study the Mutual Interference of Multiple Bodies in the Flow Field of the F-4C Aircraft in the Transonic Speed Range written by A. A. Hesketh and published by . This book was released on 1979 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index: Keyword A-L by :
Download or read book Government Reports Annual Index: Keyword A-L written by and published by . This book was released on 1986 with total page 868 pages. Available in PDF, EPUB and Kindle. Book excerpt:
