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Author :
Publisher :
ISBN 13 :
Total Pages : 314 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamic Problems Associated with V/STOL Aircraft: Propeller and rotor aerodynamics written by and published by . This book was released on 1966 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Barnes Warnock McCormick
Publisher : Courier Corporation
ISBN 13 : 9780486404608
Total Pages : 356 pages
Book Rating : 4.4/5 (46 download)
Download or read book Aerodynamics of V/STOL Flight written by Barnes Warnock McCormick and published by Courier Corporation. This book was released on 1999-01-01 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher :
ISBN 13 :
Total Pages : 275 pages
Book Rating : 4.:/5 (227 download)
Download or read book Cal/usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/stol Aircraft. Volume I. Propeller and Rotor Aerodynamics. Held June 22, 1966, Statler-hilton Hotel, Buffalo, New York written by CORNELL AERONAUTICAL LAB INC BUFFALO N Y. and published by . This book was released on 1966 with total page 275 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: A theory for static propeller performance; Propeller testing at zero velocity; Propeller research at Canadair Limited; Prediction of the performance and stress characteristics of VTOL propellers; Performance potential of rotor blade inboard aerodynamic devices; Aerodynamic loading of high-speed rotors; Prediction of rotor wake flows; The movement, structure and breakdown of trailing vortices from a rotor blade.
Author :
Publisher :
ISBN 13 :
Total Pages : 368 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamic Problems Associated with V/STOL Aircraft: Propulsion and interference aerodynamics written by and published by . This book was released on 1966 with total page 368 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher :
ISBN 13 :
Total Pages : 330 pages
Book Rating : 4.:/5 (227 download)
Download or read book Cal/usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/stol Aircraft. Volume Ii. Propulsion and Interference Aerodynamics. Held June 23, 1966, Statler-hilton Hotel, Buffalo, New York written by CORNELL AERONAUTICAL LAB INC BUFFALO N Y. and published by . This book was released on 1966 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Predicted and measured performance of two full-scale ducted propellers; Aerothermal dynamic performance of a high bypass tip turbine cruise fan system; Thrust deflection nozzles for VTOL aircraft; Shrouded propeller research at Mississippi State University leading to application on the United States Army XV-11A; The lift, drag and stability of wings immersed in propeller slipstream; Aerodynamic properties of airfoils in nonuniformly sheared flows; Experimental investigation of compound helicopter aerodynamic interference effects; Maximum lift coefficient for STOL aircraft: a critical review.
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
ISBN 13 :
Total Pages : 522 pages
Book Rating : 4.:/5 (318 download)
Download or read book The Aerodynamics of V/STOL Aircraft written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1968 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 402 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamic Problems Associated with V/STOL Aircraft: Panels on recommended V written by and published by . This book was released on 1966 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert H. Kirby
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)
Download or read book Aerodynamic Characteristics of Propeller-driven VTOL Aircraft written by Robert H. Kirby and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamic Problems Associated with V/STOL Aircraft written by and published by . This book was released on 1966 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 186 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamics of Rotary Wing and V/STOL Aircraft written by and published by . This book was released on 1969 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 792 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harry H. Heyson
Publisher :
ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.:/5 (31 download)
Download or read book Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor written by Harry H. Heyson and published by . This book was released on 1970 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt: Under sufficiently large wake deflections, the forward portion of the wake is found to flow forward along the floor leading to a vortex pattern which results in Rae's limits (Journal of Aircraft, May-June 1967). Although wind-tunnel data cannot normally be corrected successfully beyond these limits, it may be possible to obtain ground-effect data for conditions more severe than those implied by Rae.
Author : Robert C. Innis
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Flight Examination of Operating Problems of V/STOL Aircraft in STOL Type Landing and Approach written by Robert C. Innis and published by . This book was released on 1961 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 828 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Wilmer H. Reed (III.)
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Review of Propeller-rotor Whirl Flutter written by Wilmer H. Reed (III.) and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A summary is made of the state of the art of propeller-whirl flutter -- a precession-type instability that can occur on a flexibly mounted aircraft engine-propeller combination. This report reviews the literature relating to this problem from the time it first became of concern on conventional turboprop and V/STOL aircraft. Included in the survey are a description of the basic mechanism of whirl flutter, a summary of generalized trend studies on idealized systems, the status of methods for predicting propeller aerodynamic coefficients, the effects of flapping hinged blades and twisted flexible blades on whirl flutter, and some approaches for including propeller whirl modes as a part of the flutter evaluation for complete aircraft. Also, brief consideration is given to the response of flexibly mounted propeller-nacelle systems to random atmospheric turbulence. Whirl flutter of conventional propeller-nacelle systems is now a reasonably well understood phenomenon and amenable to analysis. For propeller-rotor systems with flapping blades, however, comparisons between experiment and theory suggest the need for further refinements in the mathematical model.
Author : Fritz Weinig
Publisher :
ISBN 13 :
Total Pages : 546 pages
Book Rating : 4.:/5 (89 download)
Download or read book Aerodynamics of the Propeller written by Fritz Weinig and published by . This book was released on 1948 with total page 546 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Antonio Filippone
Publisher : Elsevier
ISBN 13 : 0080461034
Total Pages : 594 pages
Book Rating : 4.0/5 (84 download)
Download or read book Flight Performance of Fixed and Rotary Wing Aircraft written by Antonio Filippone and published by Elsevier. This book was released on 2006-05-10 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more.This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft. - Unique coverage of fixed and rotary wing aircraft in a unified manner, including optimisation, emissions control and regulation. - Ideal for students, aeronautical engineering capstone projects, and for widespread professional reference in the aerospace industry. - Comprehensive coverage of computer-based solution of aerospace engineering problems; the critical analysis of performance data; and case studies from real world engineering experience. - Supported by end of chapter exercises
