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 1.

A Bibliography of NACA Reports on Control of Turbojet Engines

作      者:Sanders, John C
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 2.

A brief investigation of the effect of waves on the take-off resistance of a seaplane

作      者:Mottard, Elmo J
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 3.

A Brief Summary of Experience in Boosting Aerodynamic Research Models

作      者:Thibodaux, Joseph G , Jr
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 4.

A Description of the Ames 2- by 2-foot Transonic Wind Tunnel and Preliminary Evaluation of Wall Interference

作      者:Lawrence, Leslie F;Spiegel, Joseph M
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 5.

A Factor Affecting Transonic Leading-edge Flow Separation

作      者:Wood, George P;Gooderum, Paul B
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 6.

A flat wing with sharp edges in a supersonic stream

作      者:Donov, A E
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 7.

A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers

作      者:Kyle, Howard C;CHEATHAM DONALD C;Mathews, Charles W
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 8.

A Flight Evaluation of a Wing-shroud-blowing Boundary-layer Control System Applied to the Flaps of an F9F-4 Airplane

作      者:Rolls, L Stewart;Innis, Robert C
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 9.

A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through a Rate Type of Automatic Control System

作      者:Alford, William L;Sjoberg, S A;Russell, Walter R
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 10.

A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through an Attitude Type of Automatic Pilot

作      者:Russell, Walter R;Alford, William L;Sjoberg, S A
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 11.

A Free-flight Investigation of the Effects of a Sonic Jet on the Total-drag and Base-pressure Coefficients of a Boattail Body of Revolution from Mach Number 0.83 to 1.70

作      者:Falanga, Ralph A
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 12.

A Horizontal-tail Arrangement for Counteracting Static Longitudinal Instability of Sweptback Wings

作      者:Edwards, George G;Savage, Howard F
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 13.

A Method for Calculating the Contour of Bodies of Revolution with a Prescribed Pressure Gradient at Supersonic Speed with Experimental Verification

作      者:Burbank, Paige B
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 14.

A Method for Obtaining Statistical Data on Airplane Vertical Velocity at Ground Contact from Measurements of Center-of-gravity Acceleration

作      者:Dreher, Robert C
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 15.

A method for the design of porous-wall wind tunnels

作      者:Stokes, George M
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 16.

A method of reducing heat transfer to blunt bodies by air injection

作      者:Inouye, Momoru;Stalder, Jackson R
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 17.

A Preliminary Investigation of the Effects of Frequency and Amplitude on the Rolling Derivatives of an Unswept-wing Model Oscillating in Roll

作      者:Williams, Katherine D;Lichtenstein, Jacob H;Fisher, Lewis R
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 18.

A preliminary investigation of the static stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28

作      者:Gloria, Hermilo R;Wong, Thomas J
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 19.

A Review of Recent Information on Boundary-layer Transition at Supersonic Speeds

作      者:Seiff, Alvin
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

 20.

A semiempirical procedure for estimating wing buffet loads in the transonic region

作      者:Huston, Wilber B;Skopinski, T H
出版日期:1956
资源类型:科技报告
详细信息  原文下载:

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