Отображение 1 - 8 результаты of 8 для поиска 'Dillon, James L.,', время запроса: 0.12сек. Отмена результатов
1
Data-reduction technique for determining rapidly rising heating rates to thermally thick walls /
по Dillon, James L.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969

Government Document ‌
2
A single formula for the velocity profile through a turbulent incompressible boundary layer on a flat plate.

Thesis ‌
3
Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane /
по Dillon, James L., Pittman, Jimmy L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document ‌
4
Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane /
по Dillon, James L., Creel, Theodore R.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document ‌
5
Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane /
по Dillon, James L., Pittman, Jimmy L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document ‌
6
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
по Penland, Jim A., Hallissy, James B., Dillon, James L.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979

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Government Document ‌
7
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach number 0.2 /
по Penland, Jim A., Creel, Theodore R., Dillon, James L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document ‌
8
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
по Penland, Jim A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979
Другие авторы: “...Dillon, James L....”

Government Document ‌
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