1-24 of 25 Books
Flying Aircraft Carriers of the USAF
Flying Aircraft Carriers of the USAF
By Brian Lockett
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

Advances in Simulation of Wing and Nacelle Stall
By Rolf Radespiel,Reinhard Niehuis,Norbert Kroll,Kathrin Behrends
Wing theory in supersonic flow
Wing theory in supersonic flow
By Elie Carafoli
High Speed Wing Theory
High Speed Wing Theory
By Doris Cohen,Robert T. Jones

The Evolution of Flight
By Georg Glaeser,Hannes F. Paulus,Werner Nachtigall
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.
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
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
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
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
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
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
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
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
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
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
High Speed Wing Theory
High Speed Wing Theory
By Doris Cohen,Robert Thomas Jones

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
Morphing aerospace vehicles and structures
Morphing aerospace vehicles and structures
By John Valasek