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Author : W.L. Rodenbaugh
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book An Approach to the Evaluation of Propulsion Systems in V/STOL Aircraft by W.L.Rodenbaugh written by W.L. Rodenbaugh and published by . This book was released on 1964 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. L. Rodenbaugh
Publisher :
ISBN 13 :
Total Pages : 6 pages
Book Rating : 4.:/5 (36 download)
Download or read book An Approach to the Evaluation of Propulsion Systems in V/STOL Aircraft written by W. L. Rodenbaugh and published by . This book was released on 1964 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.X/5 (4 download)
Download or read book VTOL/STOL Aircraft written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1966 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1110 pages
Book Rating : 4.3/5 (91 download)
Download or read book The SAE Journal written by and published by . This book was released on 1964 with total page 1110 pages. Available in PDF, EPUB and Kindle. Book excerpt: Vols. 30-54 (1932-46) issued in 2 separately paged sections: General editorial section and a Transactions section. Beginning in 1947, the Transactions section is continued as SAE quarterly transactions.
Author :
Publisher :
ISBN 13 :
Total Pages : 1020 pages
Book Rating : 4.:/5 (318 download)
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1964 with total page 1020 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. Wadkovsky
Publisher :
ISBN 13 :
Total Pages : 7 pages
Book Rating : 4.:/5 (355 download)
Download or read book Analysis of Propulsion Systems for V/STOL Aircraft written by A. Wadkovsky and published by . This book was released on 1964 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : . Wadkovsky
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Analysis of Propulsion Systems for V/STOL Aircraft by A.Wadkovsky written by . Wadkovsky and published by . This book was released on 1964 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel
Publisher :
ISBN 13 :
Total Pages : 482 pages
Book Rating : 4.:/5 (318 download)
Download or read book V/STOL Propulsion Systems written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel and published by . This book was released on 1974 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Runyon H. Tindell
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book A Method for Comparing and Selecting Propulsion Systems for V/stol Aircraft by Runyon H. Tindell and John Lytttle written by Runyon H. Tindell and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 424 pages
Book Rating : 4.3/5 (91 download)
Download or read book Gas Turbine Catalog written by and published by . This book was released on 1965 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H.. Grieb
Publisher :
ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (227 download)
Download or read book Technical Evaluation Report on AGARD Technical Meeting on V/STOL Propulsion Systems written by H.. Grieb and published by . This book was released on 1974 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: ;Contents: V/STOL propulsion systems; Propulsion/airframe integration; V/STOL propulsion system components; Environmental effects; V/STOL propulsion operating experience.
Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (France)
Publisher :
ISBN 13 :
Total Pages : 450 pages
Book Rating : 4.:/5 (227 download)
Download or read book V/STOL Propulsion Systems written by ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (France) and published by . This book was released on 1974 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: Increased interest in V/STOL aircraft has led to a renewed interest in propulsion systems for these aircraft and a need to examine and formulate military requirements. The influence of the aircraft installation on the design of propulsion systems is very significant and much study is required before aircraft development can be initiated. The influence of noise requirements on engine and aircraft designs is also commanding increasing attention not only because of the awareness by both civil and military authorities over problems affecting the environment we live in, but also from the economic point of view. The high cost of aircraft and engine development, and decreased military purchases encourage consideration of civil derivatives of aircraft and engines as a means of lowering the cost of ownership. The data base provided by V/STOL propulsion system component research and the technology base obtained by operating experience with V/STOL vehicles provides an insight to the future trend of V/STOL vehicles.
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781724683373
Total Pages : 28 pages
Book Rating : 4.6/5 (833 download)
Download or read book Preliminary Study of Vto Thrust Requirements for a V/Stol Aircraft with Lift Plus Lift/Cruise Propulsion written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-06 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary assessment was made of the VTO thrust requirements for a supersonic (Type B) aircraft with a Lift plus Lift/Cruise propulsion system. A baseline aircraft with a takeoff gross weight (TOGW) of 13 608 kg (30,000 lb) was assumed. Pitch, roll, and yaw control thrusts (i.e., the thrusts needed for aircraft attitude control in the flight hover mode) were estimated based on a specified set of maneuver acceleration requirements for V/STOL aircraft. Other effects (such as installation losses, suckdown, reingestion, etc.), which add to the thrust requirements for VTO were also estimated. For the baseline aircraft, the excess thrust required for attitude control of the aircraft during VTO and flight hover was estimated to range from 36.9 to 50.9 percent of the TOGW. It was concluded that the total thrust requirements for the aircraft/propulsion system are large and significant. In order to achieve the performance expected of this aircraft/propulsion system, reductions must be made in the excess thrust requirements. Turney, G. E. and Allen, J. L. Glenn Research Center NASA-TM-81429, E-351
Author : W.J. Lewis
Publisher :
ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (11 download)
Download or read book Propulsion Systems for Advanced V/STOL Combat Aircraft written by W.J. Lewis and published by . This book was released on 1974 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. C. Tear
Publisher :
ISBN 13 :
Total Pages : 95 pages
Book Rating : 4.:/5 (227 download)
Download or read book Approaches to Determine and Evaluate the Stability of Propulsion Systems written by R. C. Tear and published by . This book was released on 1968 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: A major consideration in the current design and operation of air vehicles is the stability of the total propulsion system. The derivation of stability criteria involves many evaluations and determinations at the subcomponent level to ascertain stable operating regions and the performance coefficients that are associated with the elemental margins. Painstaking compilation of the performance and stability margin for the key flight points of operation can thus be derived and a numerical value assessed with respect to stability margin. These data, for the most part, are dependent upon empirical coefficients drawn from previous weapon system developments. As such, a major effort is warranted to define alternative approaches to the problems of stability margin assessment that will provide a likely improvement in performance for the system. Development of the capability for improved performance and defined stability margin is directly dependent on an accurately determined interface between an engine and the associated airframe. Such a determination can be achieved only if there is expert liaison between and complete cooperation by the engine and airframe development companies. The interface between such companies must be strongly developed and is extremely critical in time-phased relationships between the engine and airframe development companies.
Author : L. R. WOODWORTH
Publisher :
ISBN 13 :
Total Pages : 99 pages
Book Rating : 4.:/5 (227 download)
Download or read book The Generalized Approach to the Selection of Propulsion Systems for Aircraft written by L. R. WOODWORTH and published by . This book was released on 1951 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: The generalized approach considers the powerplant in terms of the performance and application requirements of the aircraft. A powerplant choice for a given combination of these requirements represents a compromise between powerplant weight, frontal area, and fuel consumption. Parameters relating to the performance and application requirements of aircraft are used in simplified endurance equations, which encompass a broad range of applications, in combination with powerplant characteristics. By use of electronic calculating equipment, systematic evaluation of each powerplant type and variation within type is established for each selected combination of aircraft performance and application requirements. The powerplant is selected on the basis of maximum endurance which, under the method used, is equivalent to minimum total weight of powerplant plus fuel weight. The powerplant spectrum is represented by seven powerplant types; Rocket, Ram Jet, Afterburning Turbojet, Turbojet, Ducted Fan, Turboprop with varying power division between propeller and jet, and Reciprocating. Effects of compressor pressure ratio and turbine inlet temperature on the characteristics of the gas turbine family are considered. (Author).
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (15 download)
Download or read book V/STOL propulsion systems written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
