Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396)

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Total Pages : 118 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396) by : Donald W. Ausherman

Download or read book Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396) written by Donald W. Ausherman and published by . This book was released on 1986 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Surface Pressure Measurements on a Double Delta Wing/Body Configuration at Mach 2 and Mach 3 (WTR 1396).

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Surface Pressure Measurements on a Double Delta Wing/Body Configuration at Mach 2 and Mach 3 (WTR 1396). by :

Download or read book Surface Pressure Measurements on a Double Delta Wing/Body Configuration at Mach 2 and Mach 3 (WTR 1396). written by and published by . This book was released on 1986 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The surface pressures on a clipped double-delta wing/body configuration were measured at Mach 2 and Mach 3 in the NSWC Supersonic Tunnel Number Two at angles-of-attack up to 20 deg. The winged-body model configuration has a 2-inch diameter body consisting of a 3-caliber tangent-ogive nose and and a 7-caliber cylindrical afterbody. The wing was a clipped double-delta configuration. The body had 91 pressure taps located at various axial and circumferential locations, and the wing had 47. Surface pressures were measured at several angles-of-attack for various model roll positions at both Mach 2 and Mach 3. Keywords: Double delta wing; Wing body configuration; High angle-of-attack aerodynamics.

Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396)

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ISBN 13 :
Total Pages : 190 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396) by : Donald W. Ausherman

Download or read book Surface Pressure Measurements on a Double Delta Wing/body Configuration at Mach 2 and Mach 3 (WTR 1396) written by Donald W. Ausherman and published by . This book was released on 1992 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 956 pages
Book Rating : 4.:/5 (31 download)

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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 1987 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Reports Awareness Circular : TRAC.

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ISBN 13 :
Total Pages : 564 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Reports Awareness Circular : TRAC. by :

Download or read book Technical Reports Awareness Circular : TRAC. written by and published by . This book was released on 1987-03 with total page 564 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Annual Index

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ISBN 13 :
Total Pages : 1440 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis Government Reports Annual Index by :

Download or read book Government Reports Annual Index written by and published by . This book was released on 1987 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 782 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1987 with total page 782 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Government Reports Annual Index: Keyword A-L

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ISBN 13 :
Total Pages : 1060 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Government Reports Annual Index: Keyword A-L by :

Download or read book Government Reports Annual Index: Keyword A-L written by and published by . This book was released on 1987 with total page 1060 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 520 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1988 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography

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ISBN 13 :
Total Pages : 516 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography by :

Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography written by and published by . This book was released on 1988 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1276 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Government Reports Announcements & Index by :

Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1987-04 with total page 1276 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2, 3 and 4 (WTR1421)

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ISBN 13 :
Total Pages : 254 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2, 3 and 4 (WTR1421) by : Arnold S. Collier

Download or read book Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2, 3 and 4 (WTR1421) written by Arnold S. Collier and published by . This book was released on 1986 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges by : Julio Chu

Download or read book Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges written by Julio Chu and published by . This book was released on 1996 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2,3 and 4 (WTR1421).

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2,3 and 4 (WTR1421). by :

Download or read book Surface Pressure Measurements on a Highly Swept Delta Winged Wind Tunnel Model at Mach 2,3 and 4 (WTR1421). written by and published by . This book was released on 1986 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The surface pressures of a highly swept delta winged model were measured at Mach numbers of 2, 3, and 4 in the Naval Surface Weapons Center Supersonic Tunnel No. 2 (NSWC T-2) using a commercial pressure measurement system. The Tests were performed in May of 1985. Surface pressure measurements are reported for 75 percent of the body length and the entire span of the wing for 0, 5, 10, and 15 degrees angle of attack and all roll angles from 0 to 360 degrees in 22.5 degree increments. Keywords: Surface pressures, High angle of attack, High lift to drag, Tangent ogive nosetip, Supersonic wind tunnel.

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

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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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:

Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations by : George E. Kaattari

Download or read book Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations written by George E. Kaattari and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls

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ISBN 13 :
Total Pages : 214 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls by : Louis G. Kaufman

Download or read book Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls written by Louis G. Kaufman and published by . This book was released on 1964 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure data were obtained for Mach five flows over winged re-entry configurations composed of cylindrical cabins mounted on a 60 degree sweepback delta wing with a cylindrical leading edge, clipped tips, and trailing edge flaps. The model was tested with spherical and conical fronts on the cabin, with and without tip fins, and with and without a trailing edge spoiler. Flap deflections were varied from -40 to +40 degrees and the model was pitched at angles of attack from -30 to +45 degrees for a free stream Reynolds number, based on model length of 3,575,000. (Author)