Author : Anonim
Publisher : Unknown
Page : 22 pages
File Size : 42,6 Mb
Release : 1996
Category : Electronic
ISBN : NASA:31769000702400
A Non Axisymmetric Linearized Supersonic Wave Drag Analysis Mathematical Theory
A Non Axisymmetric Linearized Supersonic Wave Drag Analysis Mathematical Theory Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of A Non Axisymmetric Linearized Supersonic Wave Drag Analysis Mathematical Theory book. This book definitely worth reading, it is an incredibly well-written.
Supersonic Flow and Shock Waves
Author : Richard Courant,K.O. Friedrichs
Publisher : Springer Science & Business Media
Page : 488 pages
File Size : 47,8 Mb
Release : 1999-02-11
Category : Mathematics
ISBN : 0387902325
Supersonic Flow and Shock Waves by Richard Courant,K.O. Friedrichs Pdf
Courant and Friedrich's classical treatise was first published in 1948 and tThe basic research for it took place during World War II. However, many aspects make the book just as interesting as a text and a reference today. It treats the dynamics of compressible fluids in mathematical form, and attempts to present a systematic theory of nonlinear wave propagation, particularly in relation to gas dynamics. Written in the form of an advanced textbook, it should appeal to engineers, physicists and mathematicians alike.
Supersonic Flow and Shock Waves
Author : Courant Richard
Publisher : Unknown
Page : 128 pages
File Size : 52,9 Mb
Release : 1901
Category : Electronic
ISBN : 0259714747
Supersonic Flow and Shock Waves by Courant Richard Pdf
IPAC-Inlet Performance Analysis Code
Author : Paul J. Barnhart
Publisher : Unknown
Page : 172 pages
File Size : 42,7 Mb
Release : 1997
Category : Electronic
ISBN : NASA:31769000705999
IPAC-Inlet Performance Analysis Code by Paul J. Barnhart Pdf
Supersonic Flow and Shock Waves
Author : Richard Courant
Publisher : Forgotten Books
Page : 300 pages
File Size : 53,7 Mb
Release : 2016-09-13
Category : Science
ISBN : 1333573308
Supersonic Flow and Shock Waves by Richard Courant Pdf
Excerpt from Supersonic Flow and Shock Waves: A Manual on the Mathematical Theory of Non-Linear Wave Motion For obvious reasons, detailed references to classified material and specific applications are not provided, and thus the table of contents may convey an impression of overemphasis on theoretical aspects. The fol lowing comments may, therefore, be made. Chapter I contains classical facts underlying any mathematical treatment of compressible flow. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.
Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag
Author : Robert L. Nelson,Clement J. Welsh
Publisher : Unknown
Page : 52 pages
File Size : 55,9 Mb
Release : 1957
Category : Aerodynamics
ISBN : UFL:31262081065681
Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag by Robert L. Nelson,Clement J. Welsh Pdf
Summary: The experimental wave drags of bodies and wing-body combinations over a wide range of Mach numbers are compared with the computed drags utilizing a 24-term Fourier series application of the supersonic area rule and with the results of equivalent-body tests.
Government Reports Announcements & Index
Author : Anonim
Publisher : Unknown
Page : 476 pages
File Size : 41,6 Mb
Release : 1996
Category : Government publications
ISBN : MINN:31951P006101293
Government Reports Announcements & Index by Anonim Pdf
Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement
Author : Kenneth Margolis,Frank S. Malvestuto,Peter J. Maxie
Publisher : Unknown
Page : 37 pages
File Size : 45,6 Mb
Release : 1957
Category : Wedges
ISBN : OCLC:249951508
Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement by Kenneth Margolis,Frank S. Malvestuto,Peter J. Maxie Pdf
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at zero lift has been carried out for a simple two-body arrangement consisting of two wedgelike surfaces, each with a rhombic lateral cross section and emanating from a common apex. Such an arrangement could be used as two stores, either embedded within or mounted below a wing, or as auxiliary bodies wherein the upper halves could be used as stores and the lower halves for bomb or missile purposes. The complete range of supersonic Mach numbers has been considered and it was found that by orienting the axes of the bodies relative to each other a given volumen may be redistributed in a manner which enables the wave drag to be reduced within the lower supersonic speed range (where the leading edge is substantially subsonic). At the higher Mach numbers, the wave drag is always increased.
Analysis of the Linearized Supersonic Flow about Pointed Bodies of Revolution by the Method of Characteristics
Author : Alan D. Sherer
Publisher : Unknown
Page : 52 pages
File Size : 40,5 Mb
Release : 1966
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106686865
Analysis of the Linearized Supersonic Flow about Pointed Bodies of Revolution by the Method of Characteristics by Alan D. Sherer Pdf
Annual Report - National Advisory Committee for Aeronautics
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 48,9 Mb
Release : 1957
Category : Aeronautics
ISBN : STANFORD:36105024166147
Annual Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
Author : C. H. Wilts,Edward W. Perkins,Isadore L. Drell,Lewis Laboratory Staff,Max. A. Heaslet,Ray H. Wright,Willard D. Coles,United States. National Advisory Committee for Aeronautics,Edmund E. Callaghan,Frank E. Belles,Franklyn B. Fuller,Leland H. Jorgensen,Virgil S. Ritchie,Albin O. Pearson,Simon C. Sommer
Publisher : Unknown
Page : 362 pages
File Size : 52,7 Mb
Release : 1958
Category : Aeronautics
ISBN : OSU:32435063879373
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4 by C. H. Wilts,Edward W. Perkins,Isadore L. Drell,Lewis Laboratory Staff,Max. A. Heaslet,Ray H. Wright,Willard D. Coles,United States. National Advisory Committee for Aeronautics,Edmund E. Callaghan,Frank E. Belles,Franklyn B. Fuller,Leland H. Jorgensen,Virgil S. Ritchie,Albin O. Pearson,Simon C. Sommer Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 1280 pages
File Size : 52,9 Mb
Release : 1984
Category : Aeronautics
ISBN : UIUC:30112075701398
Scientific and Technical Aerospace Reports by Anonim Pdf
A Few Remarks on the Limitations of Linearized Theory in Supersonic Flow
Author : Zdeněk Kopal
Publisher : Unknown
Page : 20 pages
File Size : 46,8 Mb
Release : 1947
Category : Aerodynamics, Supersonic
ISBN : WISC:89081522799
A Few Remarks on the Limitations of Linearized Theory in Supersonic Flow by Zdeněk Kopal Pdf
The Potential Theory of Unsteady Supersonic Flow
Author : John Wilder Miles
Publisher : Unknown
Page : 244 pages
File Size : 44,8 Mb
Release : 1980
Category : Aerodynamics, Supersonic
ISBN : OSU:32435066662594
The Potential Theory of Unsteady Supersonic Flow by John Wilder Miles Pdf
Technical Abstract Bulletin
Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 1766 pages
File Size : 47,5 Mb
Release : 1961-07
Category : Technology
ISBN : UTEXAS:059172131213032