Download or read book Experimental Investigation at Mach Numbers from 0 to 1 9 of Trapezoidal and Circular Side Inlets for a Fighter type Airplane written by Emmet A. Mossman and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-02 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Investigation of an 0 25 scale Inlet canard Interference Model at High Angles of Attack and Mach Numbers of 0 9 and 1 2 written by and published by . This book was released on 1974 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation at Mach Numbers from 2 1 to 3 0 of Circular Internal compression Inlets Having Translatable Centerbodies and Provisions for Boundary layer Removal written by Earl C. Watson and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1962 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation of NACA Submerged Air Inlets on a 1 5 scale Model of a Fighter Airplane written by Donald E. Gault and published by . This book was released on 1947 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cumulative Title Index to United States Public Documents 1789 1976 written by Daniel W. Lester and published by . This book was released on 1980 with total page 578 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed written by Leonard E. Stitt and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation at Mach Numbers from 2 1 to 3 0 of Circular internal contraction Inlets with Translating Centerbodies written by Emmet A. Mossman and published by . This book was released on 1956 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation at Mach Numbers from 0 80 to 1 43 of Pressure and Load Distributions Over a Thin 45 Sweptback Highly Tapered Wing in Combination with Basic and Indented Bodies written by Thomas L. Fischetti and published by . This book was released on 1957 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number range from 0.80 to 1.125 and at a Mach number of 1.43 for a 45 degree sweptback cambered wing having a thickened root, an aspect ratio of 4.0, and a taper ratio of 0.15. Data were obtained for the wing in the presence of a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2.

Download or read book Tests of a Small scale NACA Submerged Inlet at Transonic Mach Numbers written by L. Stewart Rolls and published by . This book was released on 1950 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.

Download or read book A Comparison at Mach Numbers Up to 0 92 of the Calculated and Experimental Downwash and Wake Characteristics at Various Horizonatl Tail Heights Behind a Wing with 45 Degrees of Sweepback written by Jack D. Stephenson and published by . This book was released on 1955 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation at a Mach Number of 4 95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free stream Velocity written by P. Calvin Stainback and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Experimental Investigation of a Variable area Variable internal contraction Air Inlet at Mach Numbers Between 1 42 and 2 44 written by Richard Scherrer and published by . This book was released on 1955 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Effects of Fin Plan Form on the Static Stability of Fin body Combinations at Mach Number 4 06 written by Edward F. Ulmann and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An investigation of several NACA 1 series inlets at Mach numbers from 0 4 to 1 29 for mass flow ratios near 1 0 written by Richard J. Re and published by . This book was released on 1976 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: