Download or read book Transonic Wind Tunnel Tests of A 1 15 Scale Model of the TALOS 6cl Missile written by Michael E. McDonald and published by . This book was released on 1961 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of a 1/15-scale model of the TALOS 6cl missile were performed in the TMB 7- by 10-Foot Transonic Wind Tunnel for a Mach number range of 0.7 to 1.17, at angles of attack of -4 to 10, and roll angles of 0 and -45. The investigation included evaluation of the effects of ram-air bleed at the base of the second stage and the longitudinal stability and control effectiveness of the missile. The data are presented without analysis. (Author).
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings written by R. E. DE Kuyper and published by . This book was released on 1973 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic wind tunnel tests were performed in an Calspan Corporation (formerly Cornell Aeronautical Laboratory) Eight-Foot Transonic Wind Tunnel on a missile model with canard wings. The tests were conducted during the end of April and the beginning of May, 1973. Two distinctly different investigations were made. The effect of canard wing positions, canard - tail angular orientation, canard size, model roll angle, and nose shape, were investigated during the Aerodynamic Test Phase. The use of canard wings for roll attitude control was also investigated during this phase. The effect of different jet plumes on the aerodynamic model loads were studied during the Thrust Effect Phase. A normal jet plume simulator was used and the effects of model tail position, planform, and orientation were investigated. The report presents details of the test program and the results in tabular form.
Download or read book Government Reports Announcements Index written by and published by . This book was released on 1979 with total page 1092 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Wind tunnel Test of a 24 percent Scale Model of the Bullpup b Missile written by Garland G. BRYANT and published by . This book was released on 1960 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was performed on a model of the Bullpup 'B' missile in order to determine the aerodynamic effects of various body shapes, various canard sizes and hinge locations, and a number of wing roll-tab deflections. The tests were performed over a Mach number range from 0.8 to 1.17 and an angle-of-attack range from -4 deg. to 10 deg. at roll angles of 0, 11 1/4, 22 1/2, and 45 degrees. In addition to conventional six-component force data, canard hinge moments were measured at various canard deflections. The report presents the data without analysis.(Author).
Download or read book Government Reports Annual Index written by and published by . This book was released on 1979 with total page 948 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
Download or read book Government Reports Annual Index Keyword A L written by and published by . This book was released on 1979 with total page 1324 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Wind Tunnel Tests of a Base Drag Research Missile Model written by B. F. Gorin and published by . This book was released on 1970 with total page 583 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted in order to obtain data describing the effects of various simulated rocket exhaust plumes on the model's external flow field. Data describing the flow in the nozzle exit plane and in the model boundary layer were also obtained. Model external static pressure measurements were made and Schlieren, shadowgraph and tuft photographs were taken. The tests were conducted at Mach numbers from 0.000 to 1.200 at angles of attack from -2 to +2 degrees. The report presents details of the test program, an outline of the test procedure and the results of the investigation in tabular form. (Author).
Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings written by R. E. DE Kuyper and published by . This book was released on 1973 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.
Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings Volume I written by and published by . This book was released on 1973 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic wind tunnel tests were performed in an Calspan Corporation (formerly Cornell Aeronautical Laboratory) Eight-Foot Transonic Wind Tunnel on a missile model with canard wings. The tests were conducted during the end of April and the beginning of May, 1973. Two distinctly different investigations were made. The effect of canard wing positions, canard - tail angular orientation, canard size, model roll angle, and nose shape, were investigated during the Aerodynamic Test Phase. The use of canard wings for roll attitude control was also investigated during this phase. The effect of different jet plumes on the aerodynamic model loads were studied during the Thrust Effect Phase. A normal jet plume simulator was used and the effects of model tail position, planform, and orientation were investigated. The report presents details of the test program and the results in tabular form.
Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings written by R. E. DE Kuyper and published by . This book was released on 1973 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report is Volume 2 of a three volume series. Tables of aerodynamic test data are given, including balance cavity and base pressure coefficients, axial force for aerodynamic and thrust phases, canard position, and force and moment coefficients for a series of runs.
Download or read book Wind Tunnel Tests of a One tenth Scale Model of the RP78 C Target Missile for Northrop Ventura written by William C. Noz and published by . This book was released on 1963 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of the Airplane Interference on a 0 17 scale Model of the XAAM N 4 Oriole Missile and Comparison with the Airplane Interference on a 0 17 scale Model with the XAAM N 2 Sparrow 1 Missile Part 2 Missiles in the Proximity of a 0 179 angle Model of the F4D 1 Airplane written by and published by . This book was released on 1954 with total page 313 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of the Airplane Interference on a 0 17 scale Model of the Xaam n 4 Oriole Missile and Comparison with the Airplane Interference on a 0 17 scale Model of the Xaam n 2 Sparrow i Missile Part I Missiles in the Proximity of a 0 15 scale Model of the F3h 1 Airplane written by E. M. BROWER and published by . This book was released on 1954 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of a Joined wing Missile Model written by Jennifer Corneille and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Angle Canard Missile Test in the Ames 11 foot Transonic Wind Tunnel written by Richard G. Schwind and published by . This book was released on 1978 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Third in a Series of Wind Tunnel Tests of a 0 10 scale Model of the RP76 X4 Target Missile for the Radioplane Division of Northrop Corporation written by Robert L. Baker and published by . This book was released on 1961 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
