Preliminary Investigation Of A Variable Area Auxiliary Air Intake System At Mach Numbers From 0 To 13
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Author | : Richard Scherrer |
Publisher | : |
Total Pages | : 22 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Preliminary Investigation of a Variable-area Auxiliary Air-intake System at Mach Numbers from 0 to 1.3 Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NACA Technical Publications Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 104 |
Release | : 1980 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Memorandum Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 218 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 208 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Index to NASA Technical Publications Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, Epub and Kindle
Author | : Joseph R. Milillo |
Publisher | : |
Total Pages | : 30 |
Release | : 1954 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Some Internal-flow Characteristics at Zero Flight Speed of an Annular Supersonic Inlet and an Open-nose Inlet with Sharp and Rounded Lips Book in PDF, Epub and Kindle
Static tests of an annular conical-shock inlet and an open-nose conical inlet with three lip shapes were conducted at the Langley 8-foot transonic tunnel. Measurements of pressure recovery, surface pressure, and total pressure were made through a mass-flow range extending to choking. The results indicate that the two inlets with thin sharp lips had about the same relatively poor pressure-recovery characteristics and choked at a mass-flow rate of about 78 percent of the theoretical maximum. However, both the pressure recovery and choking mass-flow rate were greatly improved by replacing the sharp lip by two alternate shapes with lip roundness and internal contraction just behind the inlet lip.
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 2106 |
Release | : 1959 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, Epub and Kindle
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author | : Clifford J. Moore |
Publisher | : |
Total Pages | : 492 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Download A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft Book in PDF, Epub and Kindle
This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.