Download or read book Reynolds Number Tests of an NPL 9510 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by Renaldo V. Jenkins and published by . This book was released on 1983 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of the NASA SC 2 0012 Airfoil in the Langley 0 3 Meter Transonic Cryogenic Tunnel written by Raymond E. Mineck and published by . This book was released on 1987 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of the NASA SC 2 0012 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by Raymond E. Mineck and published by . This book was released on 1987 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of the Cast 10 2 DOA 2 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel Phase 2 written by and published by . This book was released on 1984 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of a NASA SC 3 0712 B Airfoil in the Langley 0 3 Meter Transonic Cryogenic Tunnel written by William Garland Johnson and published by . This book was released on 1985 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1991 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Test of the Boeing Tr77 Airfoil in the Langley 0 3 Meter Transonic Cryogenic Tunnel written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-06 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: A Boeing TR77 airfoil associated with the Advanced Technology Airfoil Test (ATAT) program was tested in the Langley 0.3 m Transonic Cryogenic Tunnel. Limited analysis of the data indicated that increasing Reynolds number for a fixed Mach number resulted in increased normal-force, nose-down pitching moment, and decreased drag coefficient. Increasing Mach number while keeping the Reynolds number constant yielded the expected increase in normal-force slopes, nose-down pitching moment coefficients, and decrease in angle of attack associated with maximum normal-force coefficient. Turbulent boundary layer flow was achieved over the airfoil at low Reynolds numbers for the test Mach number range using aluminum discs. Chu, Julio and Flechner, Stuart G. and Hill, Acquilla S. and Rozendaal, Roger A. Langley Research Center...
Download or read book High Reynolds Number Transonic Tests on a NACA 0012 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by and published by . This book was released on 1987 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of the NASA SC 2 0012 Airfoil in the Langley 0 3 Meter Transonic Cryogenic Tunnel written by Raymond E. Mineck and published by . This book was released on 1987 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions from High Reynolds Number Tests of a NASA SC 3 0712 B Airfoil in the Langley 0 3 Meter Transonic Cryogenic Tunnel written by William Garland Johnson and published by . This book was released on 1985 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution from High Reynolds Number Tests of a NASA SC 3 0712 B Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by and published by . This book was released on 1985 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Studies of Condensation Effects on Airfoil Testing in the Langley 0 3 meter Transonic Cryogenic Tunnel written by Robert M. Hall and published by . This book was released on 1986 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1984 with total page 526 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions from High Reynolds Number Tests of a Boeing BAC 1 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by William G. Jr Johnson and published by . This book was released on 1985 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Test of the Boeing TR77 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by and published by . This book was released on 1990 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions from High Reynolds Number Transonic Tests of an NACA 0012 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by and published by . This book was released on 1987 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Reynolds Number Tests of a Douglas DLBA 032 Airfoil in the Langley 0 3 meter Transonic Cryogenic Tunnel written by and published by . This book was released on 1986 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
