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 1.

:A Free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements

作      者:Schult, Eugene D
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 2.

A comparative analysis of the performance of long-range hypervelocity vehicles

作      者:Eggers, Alfred J , Jr;Allen, H Julian;Neice, Stanford E
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 3.

A comparison at Mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizontal tail heights behind a wing with 45 degree of sweepback

作      者:Selan, Ralph;Stephenson, Jack D;Bandettini, Angelo
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 4.

A comparison of the hydrodynamic forces on 1/25-, 1/10-, and 8/10-size models of a Convair XF2Y-1 hydro-ski

作      者:Mcbride, Ellis E
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 5.

A comparison of the maneuvering performance of a monowing versus a cruciform missile

作      者:Schmidt, Standley F;Matthews, Howard F
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 6.

A comparison of two methods for computing the wave of wing-body combinations

作      者:Alksne, Alberta
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 7.

A Correlation of Airfoil Section Data with the Aerodynamic Loads Measured on a 45 Degree Sweptback Wing Model at Subsonic Mach Numbers

作      者:Maillard, William C;Walker, Harold J
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 8.

A Correlation of Two-dimensional Data on Lift Coefficient Available with Blowing-, Suction-, Slotted-, and Plain-flap High -lift Devices

作      者:Riebe, John M
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 9.

A discussion of methods for reducing aerodynamic heating in supersonic flight

作      者:Eggers, A J , Jr
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 10.

A discussion of recent wind-tunnel studies relating to the problems of estimating vertical- and horizontal-tail loads

作      者:Hallissy, Joseph M , Jr;Kuhn, Richard E;Stone, Ralph W , Jr
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 11.

A Drop Test for the Evaluation of the Impact Strength of Cermets

作      者:Deutsch, G C;Pinkel, B;Katz, N H
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 12.

A Dynamic-model Study of the Effect of Added Weights and Other Structural Variations on the Blade Bending Strains of an Experimental Two-blade Jet-driven Helicopter in Hovering and Forward Flight

作      者:Mccarty, John Locke;Brooks, George W
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 13.

A Flight and Analog Computer Study of Some Stabilization and Command Networks for an Automatically Controlled Interceptor During the Final Attack Phase

作      者:Triplett, William C;Turner, Howard L;White, John S
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 14.

A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds

作      者:Anderson, Seth B;Bray, Richard S
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 15.

A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 2

作      者:White, Maurice D
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 16.

A Flight Investigation at Transonic Speeds of a Model Having a Triangular Wing of Aspect Ratio 3

作      者:White, Maurice D
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 17.

A Flight Investigation at Transonic Speeds of a Model Having a Triangular Wing of Aspect Ratio 4

作      者:Bright, Loren G
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 18.

A flight investigation of the handling characteristics of a fighter airplane controlled through automatic-pilot control systems

作      者:Sjoberg, S A
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 19.

A free-flight investigation of the drag coefficients of two single-engine supersonic intercepter configurations from Mach number 0.8 to 1.90 to determine the effect of inlet and engine locations

作      者:Judd, Joseph H
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

 20.

A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50

作      者:Falanga, Ralph A
出版日期:1955
资源类型:科技报告
详细信息  原文下载:

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