Prediction Methods for Jet V/STOL Propulsion Aerodynamics. Volume I. Proceedings of a Workshop Held at the Institute for Defense Analyses, Arlington, Virginia on July 28-31, 1975


Book Description

High speed V/STOL aircraft operating from widely dispersed platforms have become of increasing interest to the U.S. Navy. The dispersed force concept requires a well developed technology base, involving phenomena and problems which do not occur on conventional aircraft or low speed V/STOL craft. Proper design must account for the interdependence of aerodynamic and propulsion phenomena, and flows so complex that purely theoretical prediction is precluded at present. A two-volume report is made on a 1975 workshop to study these interactions.







Prediction Methods for Jet V/STOL Propulsion Aerodynamics. Volume II. Proceedings of a Workshop Held at the Institute for Defense Analyses, Arlington, Virginia on July 28-31, 1975


Book Description

This volume continues the proceedings of the 1975 workshop on prediction methods for Jet V/STOL Propulsion Aerodynamics held at the Institute for Defense Analyses, Arlington, VA. This workshop was sponsored by the Naval Air Systems Command. The workshop participants included representatives from industry, government, universities and abroad.




V/STOL Aircraft Aerodynamic Prediction Methods Investigation


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.




V/STOL Aircraft Aerodynamic Prediction Methods Investigation


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


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.