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View Flying Aircraft Carriers of the USAF By Brian Lockett

Flying Aircraft Carriers of the USAF

Flying Aircraft Carriers of the USAF

By Brian Lockett

View Assessment of Wingtip Modifications to Increase the Fuel Efficiency of Air Force Aircraft By National Research Council,Division on Engineering and Physical Sciences,Air Force Studies Board,Committee on Assessment of Aircraft Winglets for Large Aircraft Fuel Efficiency

Assessment of Wingtip Modifications to Increase the Fuel Efficiency of Air Force Aircraft

Assessment of Wingtip Modifications to Increase the Fuel Efficiency of Air Force Aircraft

By National Research Council,Division on Engineering and Physical Sciences,Air Force Studies Board,Committee on Assessment of Aircraft Winglets for Large Aircraft Fuel Efficiency

View Wing Theory By Robert Thomas Jones

Wing Theory

Wing Theory

By Robert Thomas Jones

View Advances in Simulation of Wing and Nacelle Stall By Rolf Radespiel,Reinhard Niehuis,Norbert Kroll,Kathrin Behrends
Cover of Advances in Simulation of Wing and Nacelle Stall by rolf radespiel,reinhard niehuis,norbert kroll,kathrin behrends

Advances in Simulation of Wing and Nacelle Stall

By Rolf Radespiel,Reinhard Niehuis,Norbert Kroll,Kathrin Behrends

View Theory of wing sections By Ira H. Abbott
Cover of Theory of wing sections by ira h. abbott

Theory of wing sections

By Ira H. Abbott

View Wing theory in supersonic flow By Elie Carafoli

Wing theory in supersonic flow

Wing theory in supersonic flow

By Elie Carafoli

View High Speed Wing Theory By Doris Cohen,Robert T. Jones

High Speed Wing Theory

High Speed Wing Theory

By Doris Cohen,Robert T. Jones

View The Evolution of Flight By Georg Glaeser,Hannes F. Paulus,Werner Nachtigall
Cover of The Evolution of Flight by georg glaeser,hannes f. paulus,werner nachtigall

The Evolution of Flight

By Georg Glaeser,Hannes F. Paulus,Werner Nachtigall

View Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles By Cornelia Altenbuchner,Hubbard, James E., Jr.

Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles

Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles

By Cornelia Altenbuchner,Hubbard, James E., Jr.

View Basic wing and airfoil theory By Pope, Alan
Cover of Basic wing and airfoil theory by pope, alan

Basic wing and airfoil theory

By Pope, Alan

View Theory of lifting surfaces oscillating at general frequencies in a subsonic stream By Wilfred Ethelbert Aldred Acum

Theory of lifting surfaces oscillating at general frequencies in a subsonic stream

Theory of lifting surfaces oscillating at general frequencies in a subsonic stream

By Wilfred Ethelbert Aldred Acum

View Calculation of subsonic flutter derivatives for an arrowhead wing with control surfaces By Doris E. Lehrian

Calculation of subsonic flutter derivatives for an arrowhead wing with control surfaces

Calculation of subsonic flutter derivatives for an arrowhead wing with control surfaces

By Doris E. Lehrian

View Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft By C. S. Barnes

Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft

Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft

By C. S. Barnes

View Comparison of three methods for the evaluation of subsonic lifting-surface theory By Henry Clifford Garner

Comparison of three methods for the evaluation of subsonic lifting-surface theory

Comparison of three methods for the evaluation of subsonic lifting-surface theory

By Henry Clifford Garner

View Numerical appraisal of Multhopp's low-frequency subsonic lifting-surface theory By Henry Clifford Garner

Numerical appraisal of Multhopp's low-frequency subsonic lifting-surface theory

Numerical appraisal of Multhopp's low-frequency subsonic lifting-surface theory

By Henry Clifford Garner

View Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results By R. Rose

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results

By R. Rose

View Free flight measurements of the longitudinal stability of a transonic swept-winged aircraft By G. K. Hunt

Free flight measurements of the longitudinal stability of a transonic swept-winged aircraft

Free flight measurements of the longitudinal stability of a transonic swept-winged aircraft

By G. K. Hunt

View Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing By R. T. Griffiths

Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing

Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing

By R. T. Griffiths

View Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines By Derek John Raney

Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines

Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines

By Derek John Raney

View Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth By David L. I. Kirkpatrick

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth

By David L. I. Kirkpatrick

View Wing Theory By A. Robinson
Cover of Wing Theory by a. robinson

Wing Theory

By A. Robinson

View High Speed Wing Theory By Doris Cohen,Robert Thomas Jones

High Speed Wing Theory

High Speed Wing Theory

By Doris Cohen,Robert Thomas Jones

View Assessment of wingtip modifications to increase the fuel efficiency of Air Force aircraft By National Research Council Staff,Air Force Studies Board,Division on Engineering and Physical Sciences Staff
Cover of Assessment of wingtip modifications to increase the fuel efficiency of Air Force aircraft by national research council staff,air force studies board,division on engineering and physical sciences staff

Assessment of wingtip modifications to increase the fuel efficiency of Air Force aircraft

By National Research Council Staff,Air Force Studies Board,Division on Engineering and Physical Sciences Staff

View Morphing aerospace vehicles and structures By John Valasek

Morphing aerospace vehicles and structures

Morphing aerospace vehicles and structures

By John Valasek