53 resultados para Supersonic nozzles


Relevância:

10.00% 10.00%

Publicador:

Resumo:

"It is shown that adequate means are available for calculating inviscid direct and induced pressures on simple axisymmetric bodies at zero angle of attack. The extent to which viscous effects can alter these predictions is indicated. It is also shown that inviscid induced pressures can significantly affect the stability of blunt, two-dimensional flat wings at low angles of attack. However, at high angles of attack, the inviscid induced pressure effects are negligible."

Relevância:

10.00% 10.00%

Publicador:

Resumo:

Reproduced from type-written copy.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Office of Research and Development, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

National Highway Traffic Safety Administration, Office of Research and Development, Washington, D.C.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

"B-0712"--P. 33.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

Reproduced from typewritten copy.

Relevância:

10.00% 10.00%

Publicador:

Resumo:

"Contract no. Nonr 2653(00)."

Relevância:

10.00% 10.00%

Publicador:

Resumo:

"February 22, 1977."

Relevância:

10.00% 10.00%

Publicador:

Resumo:

Mode of access: Internet.