Author: Francis J. CaponePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Lift Induced on a Swept Wing by a Two-dimensional Partial-span Deflected Jet at Mach Numbers from 0.20 to 1.30
Author: Francis J. CaponePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Exploratory Investigation of Lift Induced on a Swept-wing by a Two-dimensional Partial Span Deflected Jet at Mach Numbers from 0.20 to 1.30
Author: Francis J. CaponeEffects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01
Author: Emma Jean LandrumPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 44
Book Description
The Effects on Propulsion-induced Aerodynamic Forces of Vectoring a Partial-span Rectangular Jet at Mach Numbers from 0.40 to 1.20
Author: Francis J. CaponePublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 260
Book Description
Lift-curve Slopes Determined in Flight on a Flexible Swept-wing Jet Bomber
Author: William S. Aiken (Jr.)Publisher:
ISBN:
Category : Acceleration (Mechanics)
Languages : en
Pages : 54
Book Description
An analysis is made of the effects of Mach number and dynamic pressure on the lift-curve slope of a large flexible swept-wing jet-propelled airplane by using flight measurements of normal acceleration and angle of attack with auxiliary instrumentation as needed. The methods and procedures used to correct the flight measurements (obtained in abrupt push-pull maneuvers) and to convert the flight test data to equivalent rigid conditions for comparison with rigid-model wind-tunnel tests are described in detail. The airplane angle of zero lift and the airplane-less-tail angle of zero lift for the Mach number range of the flight tests (0.42 to 0.81) are also presented. Excellent agreement was obtained in the comparison between flight and wind-tunnel rigid lift-curve slopes and angles of zero lift.
Jet-plume-induced Flow Separation on a Lifting Entry Body at Mach Numbers from 4.00 to 6.00
Author: Robert J. McGheeAerodynamics 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.
Investigation of Axisymmetric and Nonaxisymmetric Nozzles Installed on a 0.10 Scale F-18 Prototype Airplane Model
Author: Francis J. CaponeLow-Speed Wind Tunnel Testing
Author: Jewel B. BarlowPublisher: John Wiley & Sons
ISBN: 0471557749
Category : Technology & Engineering
Languages : en
Pages : 738
Book Description
A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
Analysis and Design of Flight Vehicle Structures
Author: Elmer Franklin BruhnPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008
Book Description