Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10.

Sammonds, Robert I.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...

Wind tunnel measurements of aerodynamic damping derivatives of a launch vehicle vibrating in free-free bending modes at Mach numbers from 0.70 to 2.87 and comparisons with theory /

Hanson, Perry W.
Doggett, Robert V.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Wehrend, William R.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100⁰ total-angle cone and a 10⁰ half-angle conical flare section up to a mach number of 4.08 /

Rashis, Bernard
Bond, Aleck C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga.

Hinson, William F.
Falanga, Ralph A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion ...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 /

Rumsey, Charles R.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mech...

FREE-FLIGHT MEASUREMENTS OF DRAG AND STATIC STABILITY FOR A BLUNT-NOSED 10 DEG HALF-ANGLE CONE AT MACH NUMBER 15

Compton, D. L.

April 1961

Drag and static stability for a blunt-nosed 10-deg half-angle cone in hypersonic free-fligh

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10.

Sammonds, Robert I.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...

Wind tunnel measurements of aerodynamic damping derivatives of a launch vehicle vibrating in free-free bending modes at Mach numbers from 0.70 to 2.87 and comparisons with theory /

Hanson, Perry W.
Doggett, Robert V.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Wehrend, William R.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100⁰ total-angle cone and a 10⁰ half-angle conical flare section up to a mach number of 4.08 /

Rashis, Bernard
Bond, Aleck C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga.

Hinson, William F.
Falanga, Ralph A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion ...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 /

Rumsey, Charles R.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mech...

FREE-FLIGHT MEASUREMENTS OF DRAG AND STATIC STABILITY FOR A BLUNT-NOSED 10 DEG HALF-ANGLE CONE AT MACH NUMBER 15

Compton, D. L.

April 1961

Drag and static stability for a blunt-nosed 10-deg half-angle cone in hypersonic free-fligh

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10.

Sammonds, Robert I.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...

Wind tunnel measurements of aerodynamic damping derivatives of a launch vehicle vibrating in free-free bending modes at Mach numbers from 0.70 to 2.87 and comparisons with theory /

Hanson, Perry W.
Doggett, Robert V.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Abstract

Extracted data

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Abstract

Extracted data

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