Add to ORKGThe parts of an aerodynamics research project of the Bumblebee Program, called Generalized Missile study, is described. The source related, and potential applications are discussed
Most of the aerodynamic configurations considered are suitable for highly maneuverable air-to-air or...
In order to provide experimental data for comparison with newly developed finite difference methods ...
A supersonic potential flow solver was developed to analyze the flow over complex realistic aircraft...
This report provides a brief description of those parts of an aerodynamics research project of the B...
A large amount of fundamental aerodynamic missile data, which were stored for a number of years at t...
The Bumblebee program, was designed to provide a supersonic guided missile. The aerodynamics program...
Available flow field data which can be used in validating theoretical procedures for computing flow ...
Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect rat...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Digital computer program for analysis and design of supersonic wing-body combinations, including flo...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A comprehensive test program is defined which is being implemented in the NASA/Ames 3.5 foot Hyperso...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
An integrated system of computer programs has been developed for the design and analysis of superson...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Most of the aerodynamic configurations considered are suitable for highly maneuverable air-to-air or...
In order to provide experimental data for comparison with newly developed finite difference methods ...
A supersonic potential flow solver was developed to analyze the flow over complex realistic aircraft...
This report provides a brief description of those parts of an aerodynamics research project of the B...
A large amount of fundamental aerodynamic missile data, which were stored for a number of years at t...
The Bumblebee program, was designed to provide a supersonic guided missile. The aerodynamics program...
Available flow field data which can be used in validating theoretical procedures for computing flow ...
Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect rat...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Digital computer program for analysis and design of supersonic wing-body combinations, including flo...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A comprehensive test program is defined which is being implemented in the NASA/Ames 3.5 foot Hyperso...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
An integrated system of computer programs has been developed for the design and analysis of superson...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Most of the aerodynamic configurations considered are suitable for highly maneuverable air-to-air or...
In order to provide experimental data for comparison with newly developed finite difference methods ...
A supersonic potential flow solver was developed to analyze the flow over complex realistic aircraft...