Download or read book Free flight Skin temperature and Surface pressure Measurements on a Highly Polished Nose Having a 1000 Total angle Cone and a 100 Half angle Conical Flare Section Up to a Mach Number of 4 08 written by Bernard Rashis and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Skin temperature and Surface pressure Measurements on a Highly Polished Nose Having a 1000 Total angle Cone and a 100 Half angle Conical Flare Section Up to a Mach Number of 4 08 written by Bernard Rashis and published by . This book was released on 1961 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free Flight Skin Temperature and Surface Pressure Measurements on a Highly Polished Nose Having a 100 Deg Total Angle Cone and a 10 Deg Half Angle Conical Flare Section Up to a Mach Number of 4 08 written by Bernard Rashis and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Skin temperature and Surface pressure Measurements on a Highly Polished Nose Having a 100 Degree Total angle Cone and a 10 Degree Half angle Conical Flare Section Up to a Mach Number of 4 08 written by Bernard Rashis and published by . This book was released on 1957 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: The skin temperature and surface pressure have been measured on a large-scale, highly polished nose having a relatively sharp-tipped angle. The measurements were obtained in flight from a rocket-propelled model up to a peak Mach number of 4.08 and a peak Reynolds number of 22,000,000 per foot. Temperature distributions indicated that the heating on the forward 3.5 inches of the 100 degree cone was lower than the heating on the rearward portion. Likewise, measured temperatures on the flare portion of the test nose were generally lower than the temperatures on the 100 degree cone portion. Pressure measurements on the flare portion of the nose showed that in the lower speed range the flow expands below atmospheric pressure in going from the cone to the flare; however, as the speed increased, the expansion diminished and for speeds greater than a Mach number of approximately 3.0 the flare pressure coefficients were at or near a values of zero.
Download or read book Free flight Skin temperature and Surface pressure Measurements on a Highly Polished Nose Having a 100 Total angle Cone and a 10 Half angle Conical Flare Section Up to a Mach Number of 4 08 written by Bernhard Rashis and published by . This book was released on 1961 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index of NASA Technical Publications written by and published by . This book was released on 1959 with total page 494 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat transfer Measurements in Free Flight at Mach Numbers Up to 14 6 on a Flat faced Conical Nose with a Total Angle of 29 written by Charles B. Rumsey and published by . This book was released on 1958 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerothermal Tests of a 12 50 Cone at Mach 6 7 for Various Reynolds Numbers Angles of Attack and Nose Shapes written by Robert J. Nowak and published by . This book was released on 1985 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Skin Temperature and Pressure Measurements on a Slightly Blunted 25 Degrees Cone cylinder flare Configuration to a Mach Number of 9 89 written by Aleck C. Bond and published by . This book was released on 1957 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Calibration of Conical Pressure Probes for Determination of Local Flow Conditions at Mach Numbers from 3 to 6 written by John D. Norris and published by . This book was released on 1965 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat transfer Measurements in Free Flight at Mach Numbers Up to 14 6 on a Flat faced Conical Nose with a Total Angle of 29 Degrees written by Charles B. Rumsey and published by . This book was released on 1958 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Rules of Thumb for Mechanical Engineers written by J. Edward Pope and published by Gulf Professional Publishing. This book was released on 1997 with total page 417 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fluids -- Heat transfer -- Thermodynamics -- Mechanical seals -- Pumps and compressors -- Drivers -- Gears -- Bearings -- Piping and pressure vessels -- Tribology -- Vibration -- Materials -- Stress and strain -- Fatigue -- Instrumentation -- Engineering economics.
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md and published by . This book was released on 1961 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Laminar Flow Control Technology written by and published by . This book was released on 1979 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Transition written by Tuncer Cebeci and published by Springer. This book was released on 2004 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt: Accompanying CD-ROMs include computer programs referred to in chapters 4-8 and Appendix B
Download or read book Gas Turbine Performance written by Philip P. Walsh and published by John Wiley & Sons. This book was released on 2008-04-15 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt: A significant addition to the literature on gas turbine technology, the second edition of Gas Turbine Performance is a lengthy text covering product advances and technological developments. Including extensive figures, charts, tables and formulae, this book will interest everyone concerned with gas turbine technology, whether they are designers, marketing staff or users.
Download or read book Wind Tunnels of NASA written by Donald D. Baals and published by . This book was released on 1981 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:
