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Experimental Pressure And Heat Transfer Distributions On Blunt Nose Delta Wings For Angles Of Attack Up To 30 At Mach Number 7
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Book Synopsis Experimental Pressure and Heat Transfer Distributions on Blunt-nose Delta Wings for Angles of Attack Up to 30° at Mach Number 7 by : R. Douglas Archer
Download or read book Experimental Pressure and Heat Transfer Distributions on Blunt-nose Delta Wings for Angles of Attack Up to 30° at Mach Number 7 written by R. Douglas Archer and published by . This book was released on 1963 with total page 205 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow by : Mitchel H. Bertram
Download or read book An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow written by Mitchel H. Bertram and published by . This book was released on 1963 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.
Book Synopsis Pressure Distributions on Blunt-delta Wings at Angles of Attack Up to 90 Degrees and Mach Number of 6.85 by : Peter T. Bernot
Download or read book Pressure Distributions on Blunt-delta Wings at Angles of Attack Up to 90 Degrees and Mach Number of 6.85 written by Peter T. Bernot and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Distribution on 700 Swept Slab Delta Wings at a Mach Number of 9.86 and Angles of Attack Up to 900 by : Philip E. Everhart
Download or read book Heat-transfer Distribution on 700 Swept Slab Delta Wings at a Mach Number of 9.86 and Angles of Attack Up to 900 written by Philip E. Everhart and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer distributions were obtained on 700 swept slab delta wings with sharp and blunt noses and cylindrical leading edges. The free-stream Reynolds number based on model thickness was 9 x 10(4). Lees' theory for the heat-transfer distribution is shown to be in good agreement with the data obtained on the nose and leading edge. The point of peak heating on the leading edge is in close agreement with the Newtonian stagnation point at all angles of attack. At angles of attack from 40° to 60° cross-flow theory was in excellent agreement with experimental center-line data; however, at other model attitudes the theory differed significantly from experiment. Nose blunting resulted in reduced heating rates over the aft center-line section of the wing at angles of attack less than about 40°.
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 412 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Local Pressure Distribution on a Blunt Delta Wing for Angles of Attack Up to 35 Degrees at Mach Numbers of 3.4 and 4.7 by : Marvin Kussoy
Download or read book Local Pressure Distribution on a Blunt Delta Wing for Angles of Attack Up to 35 Degrees at Mach Numbers of 3.4 and 4.7 written by Marvin Kussoy and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on 60 ̊and 70 ̊swept Delta Wings Having Turbulent Boundary Layers by : William M. Murray (Jr.)
Download or read book Heat-transfer and Pressure Distributions on 60 ̊and 70 ̊swept Delta Wings Having Turbulent Boundary Layers written by William M. Murray (Jr.) and published by . This book was released on 1966 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Design and Experimental Investigation of the FDL-5A Unmanned High L/D Spacecraft.. by : F. L. Guard
Download or read book Preliminary Design and Experimental Investigation of the FDL-5A Unmanned High L/D Spacecraft.. written by F. L. Guard and published by . This book was released on 1968 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1600 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1586 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government-wide Index to Federal Research & Development Reports by :
Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1080 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distributions on Blunt Delta Wings at a Mach Number of 2.91 and Angles of Attack Up to 90 Deg by :
Download or read book Pressure Distributions on Blunt Delta Wings at a Mach Number of 2.91 and Angles of Attack Up to 90 Deg written by and published by . This book was released on 1962 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1984 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Distribution on 70°swept Slab Delta Wings at a Mach Number of 9.86 and Angles of Attack Up to 90° by : Philip E. Everhart
Download or read book Heat-transfer Distribution on 70°swept Slab Delta Wings at a Mach Number of 9.86 and Angles of Attack Up to 90° written by Philip E. Everhart and published by . This book was released on 1964 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer distributions were obtained on 70° swept slab delta wings with sharp and blunt noses and cylindrical leading edges. The free-stream Reynolds number based on model thickness was 9 x 10(4). Lees' theory for the heat-transfer distribution is shown to be in good agreement with the data obtained on the nose and leading edge. The point of peak heating on the leading edge is in close agreement with the Newtonian stagnation point at all angles of attack. At angles of attack from 40° to 60° cross-flow theory was in excellent agreement with experimental center-line data; however, at other model attitudes the theory differed significantly from experiment. Nose blunting resulted in reduced heating rates over the aft center-line section of the wing at angles of attack less than about 40°.
Book Synopsis Calculated and Experimental Hinge Moments on a Trailing-edge Flap of a 75° Swept Delta Wing at Mach 6 by : J. Wayne Keyes
Download or read book Calculated and Experimental Hinge Moments on a Trailing-edge Flap of a 75° Swept Delta Wing at Mach 6 written by J. Wayne Keyes and published by . This book was released on 1967 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1958 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:
