A study of NACA and NASA published information of pertinence in the design of light aircraft.

Driggs, Ivan H.

April 1925

This report begins with a review and analysis of the work being done to develop light airplanes in t...

Rhode, Richard

January 1931

This report presents the results of an investigation to determine (1) the magnitude and distribution...

Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components /

Ellis, Macon C.
Grigsby, Carl E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing...

A study of NACA and NASA published information of pertinence in the design of light aircraft.

Moore, Clifford J.
Phillips, Dennis M.
Langley Research Center.
North Carolina State University. Dept. of Mechanical and Aerospace Engineering.

January 1970

This report investigates critical reviews of NACA and NASA report literature on light aircraft desig...

A study of NACA and NASA published information of pertinence in the design of light aircraft

December 1970

Three volume report contains NACA/NASA generated literature pertinent to the design of light aircraf...

A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume 3 - Propulsion subsystems, performance, stability and control, propellers, and flight safety

Moore, C. J.
Phillips, D. M.

February 1970

Critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propu...

A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume 2 - Aerodynamics and aerodynamic loads

Perkins, J. N.
Williams, J. C., III
Summey, D. C.

February 1970

Critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculation...

A summary of drag results from recent Langley full-scale-tunnel tests of Army and Navy airplanes /

Lange, Roy H.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

The results of drag investigations of twelve military airplanes tested in the Langley full-scale tun...

NACA Technical Reports

Donely, Philip

January 1950

Available information on gust structure, airplane reactions, and pertinent operating statistics has ...

NACA Technical Memorandums

March 1957

This document contains reproductions of technical papers on some of the most recent research results...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

NACA Conference on Aircraft Loads, Structures, and Flutter

March 1957

This document contains reproductions of technical papers on some of the most recent research results...

NACA Technical Reports

Crowley, J W , Jr
Green, M W

January 1929

This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...

Flight measurements of aerodynamic loads on the horizontal tail surface of a fighter-type airplane /

Garvin, John B.
United States. National Advisory Committee for Aeronautics.

January 1947

A series of flight measurements of the loads applied to the horizontal tail surfaces of a fighter-ty...

NACA Technical Reports

Diehl, Walter S.

January 1927

This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...

NACA Technical Memorandums

Driggs, Ivan H.

April 1925

This report begins with a review and analysis of the work being done to develop light airplanes in t...

NACA Technical Reports

Rhode, Richard

January 1931

This report presents the results of an investigation to determine (1) the magnitude and distribution...

Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components /

Ellis, Macon C.
Grigsby, Carl E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing...

A study of NACA and NASA published information of pertinence in the design of light aircraft.

Moore, Clifford J.
Phillips, Dennis M.
Langley Research Center.
North Carolina State University. Dept. of Mechanical and Aerospace Engineering.

January 1970

This report investigates critical reviews of NACA and NASA report literature on light aircraft desig...

A study of NACA and NASA published information of pertinence in the design of light aircraft

December 1970

Three volume report contains NACA/NASA generated literature pertinent to the design of light aircraf...

A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume 3 - Propulsion subsystems, performance, stability and control, propellers, and flight safety

Moore, C. J.
Phillips, D. M.

February 1970

Critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propu...

A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume 2 - Aerodynamics and aerodynamic loads

Perkins, J. N.
Williams, J. C., III
Summey, D. C.

February 1970

Critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculation...

A summary of drag results from recent Langley full-scale-tunnel tests of Army and Navy airplanes /

Lange, Roy H.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

The results of drag investigations of twelve military airplanes tested in the Langley full-scale tun...

NACA Technical Reports

Donely, Philip

January 1950

Available information on gust structure, airplane reactions, and pertinent operating statistics has ...

NACA Technical Memorandums

March 1957

This document contains reproductions of technical papers on some of the most recent research results...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

NACA Conference on Aircraft Loads, Structures, and Flutter

March 1957

This document contains reproductions of technical papers on some of the most recent research results...

NACA Technical Reports

Crowley, J W , Jr
Green, M W

January 1929

This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...

Flight measurements of aerodynamic loads on the horizontal tail surface of a fighter-type airplane /

Garvin, John B.
United States. National Advisory Committee for Aeronautics.

January 1947

A series of flight measurements of the loads applied to the horizontal tail surfaces of a fighter-ty...

NACA Technical Reports

Diehl, Walter S.

January 1927

This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...

NACA Technical Memorandums

Driggs, Ivan H.

April 1925

This report begins with a review and analysis of the work being done to develop light airplanes in t...

NACA Technical Reports

Rhode, Richard

January 1931

This report presents the results of an investigation to determine (1) the magnitude and distribution...

Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components /

Ellis, Macon C.
Grigsby, Carl E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing...

A study of NACA and NASA published information of pertinence in the design of light aircraft.

Abstract

Extracted data

A study of NACA and NASA published information of pertinence in the design of light aircraft.

Abstract

Extracted data

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