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Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of Accelerations in Transport-Airplane Crashes
Preston, G. Merritt & Pesman, Gerard J.
February 1958
Primary view of Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines
Ciepluch, Carl C.; North, Warren J.; Coles, Willard D. & Antl, Robert J.
April 1958
Primary view of The adhesion of molten boron oxide to various materials
Witzke, W. R.
April 1, 1958
Primary view of Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
Dryer, Murray & Luidens, Roger W.
March 18, 1958
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Hallissy, Joseph M., Jr. & Hasson, Dennis F.
August 4, 1958
Primary view of Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Carmel, Melvin M.; Kelly, Thomas C. & Gregory, Donald T.
September 10, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01
Spearman, M. Leroy & Robinson, Ross B.
March 24, 1958
Primary view of Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
Lord, Douglas R.
June 24, 1958
Primary view of Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil
Gray, Vernon H. & von Glahn, Uwe H.
February 1958
Primary view of Aerodynamic Heating of Blunt Nose Shapes at Mach Numbers Up to 14
Stoney, William E., Jr.
August 11, 1958
Primary view of Aerodynamic heating of blunt nose shapes at Mach numbers up to 14
Stoney, William E., Jr.
August 11, 1958
Primary view of Aerodynamic Load Distribution on a 45 Degree Sweptback Wing With Leading-Edge Chord-Extensions at Transonic Speeds, Including Effects of a Spoiler-Slot-Deflector Aileron
Schmeer, James W.; Whitcomb, Charles F. & West, F. E., Jr.
February 20, 1958
Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Aerodynamic Research on Fuselages with Rectangular Cross Section
Maruhn, K.
July 1958
Primary view of Altitude Performance of the Afterburner on the Iroquois Turbojet Engine. Coord. No. AF-P-6
Groesbeck, Donald E. & Peters, Daniel J.
July 28, 1958
Primary view of An Analog Study of the Influence of Internal Modifications to a Wing Leading Edge on Its Transient Temperature Rise During Highspeed Flight
Neel, Carr B.
March 17, 1958
Primary view of Analysis of effects of interceptor roll performance and maneuverability on success of collision-course attacks
Phillips, William H.
August 6, 1958
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