Author: M. F. PlatzerPublisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 548
Book Description
Prediction methods for jet V/STOL propulsion aerodynamics
Author: M. F. PlatzerPublisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 548
Book Description
V/STOL Aircraft Aerodynamic Prediction Methods Investigation
Author: Peter T. WoolerPublisher:
ISBN:
Category : Mathematical models
Languages : en
Pages : 480
Book Description
Analytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The methods take into account the strong power effects, large variations in angle of attack and sideslip, and changes in aircraft geometry that are associated with high disk loaded V/STOL aircraft operating in the aforementioned flight regimes. The theoretical development of the prediction methods is presented in this volume.
V/STOL Aircraft Aerodynamic Prediction Methods Investigation
Author: Peter T. WoolerPublisher:
ISBN:
Category : Mathematical models
Languages : en
Pages : 504
Book Description
Volume 2. Application of Prediction Methods. Final rept. 1 May 69-31 Jan 1972, FWooler, Peter T. ;Kao, Hsiao C. ;Schwendemann, Myles F. ;Wasson, Howard R. ;Ziegler, Henry ;NOR-72-9-Vol-2F33615-69-C-1602AF-698BTAFFDLTR-72-26- Vol-2See also Volume 1, AD752557 and Volume 3, AD752559.(*aerodynamic characteristics, mathematical prediction), (*short takeoff aircraft, aerodynamic characteristics), vertical takeoff aircraft, flow fields, lift, predictions, flow separation, vortices, wake, stalling, interactions, mathematical models, mapping(transformations)computer aided analysis, computer aided design, design criteriaAnalytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The aircraft configurations studied have a conventional wing, fuselage and empennage. The prediction methods are applied to a number of V/STOL configurations in this volume.
Proceedings of a Workshop on V/STOL Aircraft Aerodynamics
Author: Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 616
Book Description
V/STOL Aircraft Aerodynamic Prediction Methods Investigation
Author: Peter T. WoolerPublisher:
ISBN:
Category : Computer programs
Languages : en
Pages : 422
Book Description
Analytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The aircraft configurations studies have a conventional wing, fuselage and empennage. The prediction methods are suitable for use by design personnel during the preliminary design and evaluation of V/STOL aircraft of the type previously mentioned. Details and listings of the computer programs associated with the prediction methods are given in the volume.
Prediction Methods for Jet V/STOL Propulsion Aerodynamics
Author: Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 558
Book Description
Aerodynamics of V/STOL Flight
Author: Barnes Warnock McCormickPublisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356
Book Description
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.
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