George M. Ware

发表

Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting-Body Configuration at Mach Numbers from 0.05 to 20.3. Supplement

Christopher I. Cruz, George M. Ware, Sue B. Grafton, 1989 .

Aerodynamic predictions and experimental results for an Advanced Manned Launch System orbiter configuration

Walter C. Engelund, George M. Ware, 1993 .

Transonic aerodynamic characteristics of a proposed Assured Crew Return Capability (ACRC) lifting-body configuration

George M. Ware, 1989 .

Low-Subsonic-Speed Static Stability of Right-Triangular-Pyramid and Half-Cone Lifting Reentry Configurations

George M. Ware, 1961 .

Predicted aerodynamic characteristics for HL-20 lifting-body using the aerodynamic preliminary analysis system (APAS)

Christopher I. Cruz, George M. Ware, 1992 .

Low-Subsonic-Speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-Vehicle Configuration Having Wingtip Panels that Fold up for High-Drag Reentry

George M. Ware, 1960 .

Shuttle crew escape tube study

George M. Ware, Bernard Spencer, Andrew S. Wright, 1988 .

Aerodynamic characteristics of the HL-20 and HL-20A lifting-body configurations

George M. Ware, Bernard Spencer, John R. Micol, 1991 .

Aerodynamic characteristics of proposed assured crew return capability (ACRC) configurations

George M. Ware, Bernard Spencer, John R. Micol, 1989 .

Aerodynamic characteristics of the HL-20

Christopher I. Cruz, George M. Ware, 1993 .

Supersonic aerodynamic characteristics of a circular body Earth-to-Orbit vehicle

Roger A. Lepsch, George M. Ware, Ian O. Macconochie, 1994 .