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Book Heat transfer Measurements on a Low fineness ratio Cylinder at a Mach Number of 10 4 and Angles of Attack from 0   to 90

Download or read book Heat transfer Measurements on a Low fineness ratio Cylinder at a Mach Number of 10 4 and Angles of Attack from 0 to 90 written by Philip E. Everhart and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat transfer Measurements on a Low fineness ratio Cylinder at a Mach Number of 10 4 and Angles of Attack from 0   to 90

Download or read book Heat transfer Measurements on a Low fineness ratio Cylinder at a Mach Number of 10 4 and Angles of Attack from 0 to 90 written by Philip E. Everhart and published by . This book was released on 1967 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50     70     and 90

Download or read book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 70 and 90 written by James Larry Hunt and published by . This book was released on 1969 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1968 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Scientific and Technical Reports

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1968 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports

Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index to NASA Technical Publications

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 Degrees  70 Degrees  and 90 Degrees

Download or read book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 Degrees 70 Degrees and 90 Degrees written by James L. Hunt and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone cylinder flare Configuration in Free Flight at Mach Numbers Up to 4 7

Download or read book Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone cylinder flare Configuration in Free Flight at Mach Numbers Up to 4 7 written by Charles R. Rumsey and published by . This book was released on 1961 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Measurements of Aerodynamic Heat Transfer and Boundary layer Transition on a 10   Cone in Free Flight at Supersonic Mach Numbers Up to 5 9

Download or read book Measurements of Aerodynamic Heat Transfer and Boundary layer Transition on a 10 Cone in Free Flight at Supersonic Mach Numbers Up to 5 9 written by Charles B. Rumsey and published by . This book was released on 1956 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: Aerodynamic heat-transfer measurements were at six stations on the 40-inch-long 10° total-angle conical nose of a rocket-propelled model which was flight tested at Mach numbers up to 5.9. The range of local Reynolds number was from 6.6 x 106 to 55.2 x 106. Laminar, transitional, and turbulent heat-transfer coefficients were measured, and, in general, the laminar and turbulent measurements were in good agreement with theory for cones. Experimental transition Reynolds numbers varied from less than 8.5 x 106 to 19.4 x 106. At a relatively constant ratio of wall temperature to local static temperature near 1.2, the transition Reynolds number increased from 9.2 x 106 to 19.4 x 106 as Mach number increased from 1.57 to 3.38. At Mach numbers near 3.7, the transition Reynolds number decreased as the skin temperature increased toward adiabatic wall temperatures.

Book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50    70    and 90

Download or read book Heat Transfer to the Windward Side of a Fineness ratio 2 9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 70 and 90 written by James L. Hunt and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Free flight Measurements of Aerodynamic Heat Transfer to Mach Number 3 9 and of Drag to Mach Number 6 9 of a Fin stabilized Cone cylinder Configuration

Download or read book Free flight Measurements of Aerodynamic Heat Transfer to Mach Number 3 9 and of Drag to Mach Number 6 9 of a Fin stabilized Cone cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1966 with total page 2088 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA SP

    Book Details:
  • Author :
  • Publisher :
  • Release : 1962
  • ISBN :
  • Pages : 436 pages

Download or read book NASA SP written by and published by . This book was released on 1962 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt: