Author: Gordon E. Osterstrom Publisher: ISBN: Category : Combustion Languages : en Pages : 66
Book Description
This report support simultaneous direct and schlieren photographs at 40,000 frames a second and correlated pressure records taken of knocking combustion in a special spark-ignition engine to ascertain intensity of certain end-zone reactions previously seen by schlieren photography alone.
Author: Warren A. Tucker Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 738
Book Description
A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By restriction to case for which Mach lines from wing apex lie behind the leading edge, a simplified treatment was possible; results of previous work on lift of triangular wings could be used to derive expressions for lift effectiveness, pitching moment, rolling-moment effectiveness, hinge moment due to control deflection, and hinge moment due to angle of attack. Comparisons were made with two-dimensional case.
Author: Gordon E. Osterstrom
Author: Benjamin Pinkel
Author: Gordon E. Osterstrom
Author: Gordon E. Osterstrom
Author: Gordon E. Osterstrom
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: Warren A. Tucker
Author: 
Author: United States. National Advisory Committee for Aeronautics