A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Sweptback Wing Body Combination Designed For High Performance
DOWNLOAD
Download A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Sweptback Wing Body Combination Designed For High Performance PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Sweptback Wing Body Combination Designed For High Performance book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance
DOWNLOAD
Author : Donald L. Loving
language : en
Publisher:
Release Date : 1961
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance written by Donald L. Loving and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.
Nasa Technical Note
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1961
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
Investigation At Mach Numbers From 0 80 To 1 43 Of Pressure And Load Distributions Over A Thin 45 Sweptback Highly Tapered Wing In Combination With Basic And Indented Bodies
DOWNLOAD
Author : Thomas L. Fischetti
language : en
Publisher:
Release Date : 1957
Investigation At Mach Numbers From 0 80 To 1 43 Of Pressure And Load Distributions Over A Thin 45 Sweptback Highly Tapered Wing In Combination With Basic And Indented Bodies written by Thomas L. Fischetti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamic load categories.
Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number range from 0.80 to 1.125 and at a Mach number of 1.43 for a 45 degree sweptback cambered wing having a thickened root, an aspect ratio of 4.0, and a taper ratio of 0.15. Data were obtained for the wing in the presence of a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2.
Publications Announcements
DOWNLOAD
Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1958
Publications Announcements written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.
A Supersonic Area Rule And An Application To The Design Of A Wing Body Combination With High Lift Drag Ratios
DOWNLOAD
Author : Richard T. Whitcomb
language : en
Publisher:
Release Date : 1960
A Supersonic Area Rule And An Application To The Design Of A Wing Body Combination With High Lift Drag Ratios written by Richard T. Whitcomb and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Airplanes categories.
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body combinations at moderate supersonic speeds with axial developments of cross-sectional area has been derived. The wave drag of a combination at a given supersonic speed is related to a number of developments of cross-sectional areas as intersected by Mach planes. On the basis of this concept and other design procedures, a structurally feasible, swept-wing--indented-body combination has been designed to have relatively high maximum lift-drag ratios over a range of transonic and moderate supersonic Mach numbers. The wing of the combination has been designed to have reduced drag associated with lift and, when used with an indented body, to have low zero-lift wave drag. Experimental results have been obtained for this configuration at Mach numbers from 0.80 to 2.01. Maximum lift-drag ratios of approximately 14 and 9 were measured at Mach numbers of 1.15 and 1.41, respectively.
Nasa Technical Report
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1960
Nasa Technical Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics categories.
Monthly Catalog Of United States Government Publications Cumulative Index
DOWNLOAD
Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1979
Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with United States categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1959
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aeronautics categories.
Index Of Nasa Technical Publications
DOWNLOAD
Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960
Index Of Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.
Monthly Catalog Of United States Government Publications
DOWNLOAD
Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1961
Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Government publications categories.