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The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight (Report / United States. National Advisory Committee for Aeronautics)

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The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight (Report / United States. National Advisory Committee for Aeronautics)

Frank M Hamaker

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The Similarity Law for Hypersonic Flow About Slender Three-Dimensional Shapes

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The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight (Report / United States. National Advisory Committee for Aeronautics)

The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight (Report / United States. National Advisory Committee for Aeronautics)

More Books

Analysis of solar radiation sheilds for temperature control of space vehicles subjected to large changes in solar energy / by George J. Nothwang, John C. Arvesen and Frank M. Hamaker. [Leather Bound]

Analysis of solar radiation sheilds for temperature control of space vehicles subjected to large changes in solar energy / by George J. Nothwang, John C. Arvesen and Frank M. Hamaker. [Leather Bound]

Effectiveness of radiation shields for thermal control of vehicles on the sunlit side of the moon / John C. Arvesen and Frank M. Hamaker. 1964 [Leather Bound]

Effectiveness of radiation shields for thermal control of vehicles on the sunlit side of the moon / John C. Arvesen and Frank M. Hamaker. 1964 [Leather Bound]

Temperature recovery factors on a slender 12À cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45À / by John O. Reller, Jr., and Frank M. Hamaker. 1955 [Leather Bound]

Temperature recovery factors on a slender 12À cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45À / by John O. Reller, Jr., and Frank M. Hamaker. 1955 [Leather Bound]

The Similarity Law for Hypersonic Flow About Slender Three-Dimensional Shapes

The Similarity Law for Hypersonic Flow About Slender Three-Dimensional Shapes